CN103352755B

CN103352755B - A kind of internal combustion engine

Info

Publication number: CN103352755B
Application number: CN201310320247.7A
Authority: CN
Inventors: 不公告发明人
Original assignee: Individual
Current assignee: Individual
Priority date: 2013-07-29
Filing date: 2013-07-29
Publication date: 2015-10-21
Anticipated expiration: 2033-07-29
Also published as: CN103352755A

Abstract

The invention provides a kind of technological scheme of internal combustion engine, by rotor of calming the anger, acting rotor, firing chamber, fuel supplying device, ignition mechanism is formed, rotor of calming the anger with acting rotor in body on same axis, the combined type acting rotor of acting rotor is made up of turbine-type turbine and non-turbine-type impeller, chamber, bowl-type whirlpool is had before turbine-type turbine, after have guide plate and power turbine, main exhaust, chamber, whirlpool there is bypass air flue, non-turbine-type impeller cavity there are return-air road and secondary air outlet flue, return-air road is communicated with chamber, whirlpool, non-turbine-type impeller there is up and down tongue piece, cylindrical piston is had in firing chamber, piston centre has fumarole, in fumarole, fuel injector is installed, piston rear end has piston position controller, firing chamber rear chamber rear end is communicated with rotor air outlet of calming the anger, firing chamber front chamber front end is communicated with combined type acting rotor main extra-air inlet, described primary air inlet is communicated with non-turbine-type impeller cavity, described extra-air inlet is communicated with chamber, whirlpool.

Description

A kind of internal combustion engine

Technical field

What the present invention relates to is a kind of turbogenerator, especially a kind of turboshaft engine.

Background technique

In the prior art, the technology the most close with the application is that the free turbine airscrew engine in gas turbine engine also claims turbo oar engine, free turbine Duct-Burning Turbofan also claims turbofan engine and turboaxle motor also to claim turboshaft engine, all turboshaft engine is called for short in describing once for simplicity, turboshaft engine is all to be calmed the anger the power turbine of rotor by the primary and secondary turbine that does work, adopt time final stage acting turbine rate of doing work output rotor, the high-temperature high-pressure fuel gas sprayed in firing chamber as you know its energy after the elementary turbine acting of impact is decayed step by step, the maximum kinetic energy of acting combustion gas acts on primary and secondary acting turbine, that is the kinetic energy that the middle primary and secondary that works acting turbine produces is maximum, the power taken at work due to whole rotor of calming the anger is smaller, turboshaft engine primary and secondary acting turbine as rotor of calming the anger power turbine its to arrange in the quantity of progression and be subject to significant limitation, because of the end of turbine at whole combustion gas acting passage that do work as the secondary final stage of output power, progression has arranged many will affect power stage, also have, although turboshaft engine has carried out split axle compression and combustion with power stage also claim free turbine, but it is at different levels all on the same axis as the secondary final stage acting turbine of power stage, can not independence and freedom running be the equal of only single-stage freewheel between at different levels, effect and the efficiency of its classification are lower, besides in order to ensure enough rotating speeds and torsion output, the combustion gas acted on time final stage acting turbine just must have sufficiently high pressure and temperature, gaseous-pressure after this just makes time final stage turbine and temperature can not be fallen, because high-temperature high-pressure fuel gas can not convert mechanical energy to completely on single freewheel, cause the exhaust gas temperature after doing work and flow velocity also just still very high, this part energy is by slatterning in vain, farthest can not absorb the energy that high-temperature high-pressure fuel gas produces, fuel utilization efficiency is low, the acting rotor also having turboshaft engine is all that is turbine-type turbine can only operate under a kind of mode of operation and turbine-type turbine pattern, when the characteristic of turbine is high rotary speed working, efficiency is higher, slow-speed of revolution work limitation rate is very low, slow-speed of revolution requirements of one's work cannot be adapted in a kind of mode of operation, also have the rotating ratio in turboshaft engine between compressor turbine and acting turbine can not change according to the change of operating mode, its power stage scope and operating mode accommodation relative narrower, these defects of turboshaft engine cause its reason that oil consumption is higher when the slow-speed of revolution works, be exactly the size of its puff prot in addition, the shape of firing chamber, volume all immobilizes, make fuel from injection, mixing, igniting, the distance being burned to acting rotor all immobilizes, make fuel Applicable scope relative narrower, pluralities of fuel can not better be used, the deficiency that Here it is existing for prior art.

Summary of the invention

Technical problem to be solved by this invention, be exactly for the deficiency existing for prior art, and provide a kind of primary and secondary the highest by kinetic energy to do work turbine output rate by calming the anger the power turbine of rotor by secondary final stage acting turbine that operates of independence and freedom, primary and secondary acting turbine and time final stage acting turbine can independent operation, power stage turbine is arranged more reasonable unrestricted on progression arranges at the power turbine of rotor of front calming the anger at rear its, the power turbine of rotor of calming the anger is at different levels all can independence and freedom running, can with different rotation speed operation, the rotor of calming the anger strengthened step by step is with the combustion gas just in time perfect matching of decaying step by step, can farthest absorb combustion gas energy, make exhaust temperature, flow velocity is lower, efficiency is higher, also the shape of combuster and do work rotor and the rotating ratio of calming the anger between rotor all can regulate and control along with the change of operating mode automatically, accomplish adjustable variable controllable, and can in turbine pattern, non-turbine pattern, work under the multiple-working modes such as mixed mode, rotating speed Applicable scope is wider, power stage scope is higher, can in high speed, work under low speed and complex working conditions, the internal-combustion engine technology scheme that multi fuel exchanges can be realized when not changing machine hardware.

This programme is achieved by the following technical measures: primarily of body, to calm the anger rotor, acting rotor, firing chamber and fuel supplying device and ignition mechanism are formed, described rotor of calming the anger is arranged in body respectively with acting rotor calms the anger in rotor chamber and acting rotor chamber, described rotor of calming the anger with acting rotor in body on same axis, described rotor of calming the anger is made up of centrifugal compressor turbine and charging turbine, described centrifugal compressor turbine can be one, the multistage centrifugal compressor turbine that two or more centrifugal compressor turbine is formed, described charging turbine can be one, the multi-stage booster turbine that two or more charging turbine is formed, described centrifugal compressor turbine is followed between charging turbine and can separately also can be connected through planetary gear set between charging turbine at different levels, described acting rotor is made up of combined type acting rotor and power turbine, described combined type acting rotor is by conical wheel body, turbine-type turbine, non-turbine-type impeller is formed, the conical wheel body of described combined type acting rotor is arranged on acting rotor shaft rear end, described conical wheel body end outer week is turbine-type turbine, described turbine-type turbine excircle is non-turbine-type blade wheel structure, described power turbine can be one, two or more free power turbine forms turbine flow, described combined type acting rotor is followed between elementary power turbine and can separately also can connect through planetary gear set between power turbine at different levels, the chamber, bowl-type whirlpool matched with turbine-type turbine diameter is had before the turbine-type turbine of described combined type acting rotor, described acting rotor shaft front end is passed bowl-type Wo Qiang bottom centre and is connected with rotor shaft rear end of calming the anger and connect power output shaft through gear train, described acting rotor shaft is same center line with rotor shaft of calming the anger, described centrifugal compressor turbine is arranged on rotor shaft front end of calming the anger, described charging turbine is arranged on supercharging rotor shaft front end, described supercharging rotor shaft rear end to be contained in rotor beam barrel of calming the anger through centrifugal compressor turbine central sleeve and to pass acting rotor shaft rear end, described power turbine is arranged on the rear end of the supercharging rotor shaft passed with acting rotor shaft center through rotor shaft of calming the anger, described charging turbine can be the multi-stage booster turbine be made up of multiple charging turbine, described power turbine can be the turbine flow be made up of multiple power turbine, the first charging turbine in described multi-stage booster turbine is arranged on the first supercharging rotor shaft front end, described first supercharging rotor shaft rear end through centrifugal compressor turbine center and to be sleeved in the beam barrel of rotor shaft of calming the anger and to pass the rear end of acting rotor shaft and the first power turbine is installed, second charging turbine is arranged on the second supercharging rotor shaft front end, described second supercharging rotor shaft rear end through the first charging turbine center and to be sleeved in the beam barrel of the first supercharging rotor shaft and after passing the first supercharging rotor shaft, the second power turbine to be installed, 3rd charging turbine is arranged on the 3rd supercharging rotor shaft front end, the rear end of described 3rd supercharging rotor shaft to be contained in the beam barrel of the second supercharging rotor shaft through the second charging turbine central sleeve and to be provided with the 3rd power turbine after passing the second supercharging rotor beam barrel, charging turbines at different levels in described multi-stage booster turbine are arranged on the front end of supercharging rotor shaft at different levels successively, the rear end of described supercharging rotor shaft at different levels to be contained in the beam barrel of prime supercharging rotor shaft through prime charging turbine central sleeve and to be provided with corresponding power turbine at the corresponding levels after passing prime supercharging rotor beam barrel, that is the first order charging turbine (in order to be convenient to describe hereinafter referred to as charging turbine in an embodiment) in the charging turbines at different levels in the multi-stage booster turbine be made up of multiple charging turbine and the turbine flow be made up of multiple power turbine is arranged on first order supercharging rotor shaft (hereinafter referred to as supercharging rotor shaft) front end, described supercharging rotor shaft rear end is contained in rotor beam barrel of calming the anger through centrifugal compressor turbine central sleeve and passes acting rotor shaft rear end and install first order power turbine (hereinafter referred to as power turbine), second level charging turbine is arranged on supercharging rotor shaft front end, the second level, described second level supercharging rotor shaft rear end is contained in supercharging rotor beam barrel through charging turbine central sleeve and passes the installation second level, supercharging rotor shaft rear end power turbine, 3rd charging turbine is arranged on the 3rd supercharging rotor shaft front end, described 3rd supercharging rotor shaft rear end to be contained in the second supercharging rotor beam barrel through the second charging turbine central sleeve and to pass the second supercharging rotor shaft rear end and is provided with the 3rd power turbine, its supercharging rotor at different levels is arranged on the front end of supercharging rotor shaft at different levels by that analogy, supercharging rotor shaft at different levels is provided with power turbine at the corresponding levels through after adjacent prime supercharging rotor shaft from adjacent prime supercharging rotor shaft center backward, charging turbine at different levels matches and independent operation mutually with power turbine at different levels, at centrifugal compressor turbine with between charging turbine and between charging turbine at different levels, the turbine-type turbine of combined type acting rotor is followed between power turbine and has guiding piece and hollow spacer dish between power turbine at different levels, calm the anger rotor shaft with between supercharging rotor shaft and acting rotor shaft with between supercharging rotor shaft and have the lubrication of spring bearing and seal ring and routine to arrange between supercharging rotor shaft at different levels, the main exhaust matched with final stage power turbine diameter is had after the final stage power turbine of turbine flow, combuster on combined type acting rotor, described firing chamber there are fuel supplying device and ignition mechanism, rear end, described firing chamber communicates with rotor air outlet of calming the anger, described chamber front end has combined type acting rotor main suction port and extra-air inlet, described combined type acting rotor main suction port and extra-air inlet can be equipped with master air suction valve and secondary suction valve respectively, described primary air inlet communicates with non-turbine-type impeller cavity on the non-turbine-type impeller cavity upper semi-circle of combined type acting rotor, described extra-air inlet is communicated with the chamber, whirlpool before the turbine-type turbine of combined type acting rotor, the lower semi-circle that described combined type acting rotor non-turbine-type impeller cavity suction port is relative there is acting rotor air outlet, described acting rotor air outlet there is return-air road and communicates, described return-air road is communicated with the chamber, whirlpool before combined type acting rotor turbine-type turbine, chamber, whirlpool before described combined type acting rotor turbine-type turbine is through turbine-type turbine, power turbine communicates with the main exhaust after final stage power turbine.Described acting rotor and calm the anger between rotor and have interval body wall, spring bearing is had in described body wall, described body also has other supplementary equipment, the acting rotor air outlet that primary air inlet is corresponding can also there is secondary air outlet flue, the external secondary air outlet flue in described acting rotor air outlet there is outlet valve, described secondary air outlet flue communicates with main exhaust through outlet valve, described supercharging rotor can be the various forms of gas pressure mechanisms being applicable to this programme in prior art, as centrifugal turbocompressor, blade pump type gas compressor or turbine-type turbocompressor etc., described rotor of calming the anger can be the single-stage be made up of single rotor of calming the anger structure of calming the anger also can be two-stage that two compressor turbines are formed structure of calming the anger can also be the multistage compressor structure that multiple rotor of calming the anger is formed, as multistage turbine fan-type gas compressor, multistage turbine formula turbocompressor, multistage blade pump type gas compressor etc., described rotor of calming the anger can also be the combined multi-stage gas pressure mechanism that the gas compressor of various ways is formed, as made primary and secondary gas compressor with turbine hinge formula multistage compressor, centrifugal turbocompressor is final stage gas compressor, centrifugal turbocompressor is elementary gas compressor, blade pump type gas compressor is the mixed construction such as middle final stage gas compressor, described multistage compressor structure or combined multi-stage gas pressure mechanism at different levels between can be split axle pattern also can be that selectively to use planetary gear set to carry out connection coaxial, split axle is used with, specifically can select integrated mode flexibly according to actual needs, described planetary gear set can be the planetary gear set of single cover also can be the planetary pinion combination that many cover planetary pinions are formed, described planetary gear set can there is planetary gear set control gear, described planetary gear set control gear can lock wantonly two gears in planetary gear set also locking or control can be in that gear of free state.Described acting rotor shaft is followed between supercharging rotor shaft and is had spring bearing between supercharging rotor shaft at different levels.Described acting rotor shaft front end passes directly can connect into concentric shafts with rotor shaft rear end of calming the anger from bowl-type Wo Qiang bottom centre, described concentric shafts connects with power output shaft through gearing, described gearing can be by basin tooth, the gear train that cone tooth is formed, also can be by basin tooth, cone tooth, the gear train that general gear is formed, it can also be any Gear combination being applicable to this programme in prior art, described acting rotor shaft front end passes from bowl-type Wo Qiang bottom centre and to connect with rotor shaft rear end of calming the anger by planetary gear set afterwards, described planetary gear set can there is planetary gear set control gear, as: in the planetary carrier that acting rotor shaft front end is connected in planetary gear set in the heart, to calm the anger in sun gear that rotor shaft rear end is connected in planetary gear set in the heart, the bull gear of power in planetary gear set, gearing, power output shaft exports.As: in the sun gear side that acting rotor shaft front end is connected in planetary gear set in the heart, to calm the anger in sun gear opposite side that rotor shaft rear end is connected in planetary gear set in the heart, planetary carrier in planetary gear set is controlled, and the bull gear of power in planetary gear set, gearing, power output shaft export.As: in the sun gear side that acting rotor shaft front end is connected in planetary gear set in the heart, to calm the anger in sun gear opposite side that rotor shaft rear end is connected in planetary gear set in the heart, bull gear in planetary gear set is controlled, and the planetary carrier of power in planetary gear set, gearing, power output shaft export.As:, rotor shaft rear end of calming the anger to be connected in the sun gear in planetary gear set in the heart, and the planetary carrier of power in planetary gear set, gearing, power output shaft export in the bull gear that acting rotor shaft front end is connected in planetary gear set in the heart.Described planetary gear set can also be any planetary pinion combination that can be used for this programme.Before the turbine-type turbine of described combined type acting rotor, chamber, bowl-type whirlpool has bypass air flue to communicate with calm the anger rotor air outlet and air, described bypass air flue has bypass valve with rotor air outlet connectivity part of calming the anger, described bypass air flue can connect calming the anger on rotor final stage air outlet with the connection interface of rotor of calming the anger, also can any one-level in the multistage compressor of calming the anger rotor connect, the gas port that described bypass air flue follows air to communicate there is one-way valve, described non-turbine-type impeller can be unshrouded impeller also can be blade is while by the single shrouded wheel of wheel sheet shutoff or blade both sides all by the double shrouded wheel of wheel sheet shutoff, blade on described non-turbine-type impeller is fixed on wheel body, described blade can tilt also can tilt counterclockwise in the past clockwise in the past, can have with blade with wide and can be up and down tongue piece between adjacent two blades on described non-turbine-type impeller, a limit of described tongue piece is carried out activity with a blade top margin in adjacent two blades with movable axis and is connected, described movable axis can also can on the clockwise side top margin of blade on the counterclockwise side top margin of blade, described tongue piece is that the blade face of another edge, axle center another blade adjacent slides up and down within the scope of 90 degree with coupling shaft, its top dead center is no more than corresponding blade top margin, its radian of blade face camber corresponding to described tongue piece active edges and the slip radian of tongue piece sliding edge match, in unshrouded impeller structure when tongue piece sliding edge is at top dead center adjacent two blades, tongue piece, the rotor cavity of an opposing seal is formed between the inner circumference at blade place and combined type acting rotor non-turbo wheel chamber two wall, in double shrouded wheel structure when tongue piece sliding edge is at top dead center adjacent two blades, tongue piece, the rotor cavity of an opposing seal is formed between the inner circumference at blade place and blade two side wheel sheet, in semi-closed type impeller structure, adjacent two blades when tongue piece active edges is at top dead center, tongue piece, the impeller cavity of an opposing seal is formed between the wheel chamber sidewall of the inner circumference at blade place and blade wheel sheet on one side and blade another side, below described combined type acting rotor non-turbine-type impeller cavity suction port, sidewall have with circular arc air inlet duct corresponding to chamber, bowl-type whirlpool circular arc degree, lower semi-circle sidewall has corresponding circular arc outgassing groove, chamber, whirlpool before described combined type acting rotor turbine-type turbine has bypass air flue to communicate with calm the anger rotor air outlet and air, described bypass air flue communicates with rotor air outlet of calming the anger through bypass valve, described bypass air flue there is one-way valve with the air place of communicating, secondary fuel injector is had on described bypass valve internal bypass air flue He on secondary intake duct, described secondary fuel injector is communicated with fuel supplying device, pore is had to follow the circular arc outgassing groove on combined type acting rotor non-turbine-type impeller cavity sidewall and circular arc air inlet duct to communicate bottom described rotor cavity, described outgassing groove communicates with chamber, bowl-type whirlpool, described air inlet duct is communicated with between one-way valve and bypass valve with the bypass air flue in chamber, bowl-type whirlpool, the air flue that described air inlet duct follows bypass air flue to communicate there is one-way valve, the air flue that described outgassing groove follows chamber, whirlpool to communicate there is one-way valve.Pore is had to follow corresponding circular arc outgassing groove and circular arc air inlet duct on combined type acting rotor non-turbine-type impeller cavity sidewall to communicate bottom described rotor cavity, described outgassing groove can the combined type in main exhaust side do work on rotor non-turbine-type impeller cavity sidewall, described air inlet duct is on the opposite side combined type acting rotor non-turbine-type impeller cavity sidewall of correspondence, described outgassing groove can the combined type in side, chamber, bowl-type whirlpool do work on rotor non-turbine-type impeller cavity sidewall, described air inlet duct is on the opposite side combined type acting rotor non-turbine-type impeller cavity sidewall of correspondence, described air inlet duct and outgassing groove can coexist on the combined type acting rotor non-turbine-type impeller cavity sidewall of side, spring can be had in rotor cavity below described tongue piece, above described combined type acting rotor, body there is throat less chamber, the cylindrical piston matched with firing chamber inner circle is had in described firing chamber, described cylindrical piston is divided into former and later two chambers firing chamber, cylindrical piston slides in the front and back chamber of firing chamber, described cylindrical piston periphery there is sealed piston ring, there is fumarole at described cylindrical piston center, described fumarole can there is vortex shape guiding piece also can have helical guide channel, in described fumarole, fuel injector is installed, described fuel injector front and back in fumarole slide axially, described fuel injector in fumarole during front position the aperture of fumarole minimum, described fuel injector in fumarole during rearmost position the aperture of fumarole maximum, there is piston position controller described cylindrical piston rear end, described piston position controller can advance or retract piston control piston position residing in firing chamber, telescopic pipe is had in described firing chamber rear chamber, described telescopic pipe front end is connected on fuel injector and communicates with fuel injector, telescopic pipe rear end is through piston position controller, body communicates with body outer fuel supplier, described telescopic pipe can control the aperture size of fumarole and then controls the spray air flow of fumarole in the position of fuel metering sparger in fumarole, can there be spring described cylindrical piston rear end with between piston position controller, described firing chamber rear chamber rear end is communicated with rotor air outlet of calming the anger, described firing chamber front chamber front end is communicated with extra-air inlet with the combined type epitrochanterian primary air inlet that does work, described firing chamber front chamber front end is built with ignition mechanism, can there be gas-separating valve in primary air inlet and the extra-air inlet intersection of described combined type acting rotor, when described gas-separating valve closes primary air inlet completely, extra-air inlet is in complete opening state, when described gas-separating valve closes extra-air inlet completely, primary air inlet is in complete opening state, described combined type acting rotor main suction port and extra-air inlet can be equipped with master air suction valve and secondary suction valve replacement gas-separating valve respectively, described primary air inlet communicates with the non-turbine-type impeller cavity of combined type acting rotor, described extra-air inlet is communicated with the chamber, whirlpool before combined type acting rotor turbine-type turbine, the lower semi-circle that described combined type acting rotor non-turbine-type impeller cavity suction port is relative there is acting rotor air outlet, described acting rotor air outlet can in non-turbine-type impeller cavity lower semi-circle circumferentially, also can on the sidewall of non-turbine-type impeller cavity lower semi-circle, there is return-air road at described acting rotor air outlet place, described return-air road communicates with the chamber, whirlpool before combined type acting rotor turbine-type turbine, described return-air road there is return-air valve, chamber, whirlpool before described combined type acting rotor turbine-type turbine is through turbine-type turbine, power turbine at different levels communicates with the main exhaust after final stage power turbine, described acting rotor air outlet can there is secondary air outlet flue and communicate with secondary air outlet flue, outside return-air road, place, described acting rotor air outlet, secondary air outlet flue there is outlet valve, described fuel supplying device can be the fuel-supplying unit that can supply various liquid fuel and gaseous fuel being applicable to this programme in prior art, described fuel injector, secondary fuel injector can be applicable to the fuel nozzle that can spray various gas and liquid fuel of this programme or shower nozzle or other fuel injector part in prior art, described ignition mechanism can be the various ignition devices that can be used for this programme in prior art, described combined type acting rotor can be single combined type acting rotor also can be two combined types acting rotors can also be two or more multiple combined type acting rotor, when described combined type acting rotor is two, two combined type acting rotors can share a firing chamber and also can not share a firing chamber, when described combined type acting rotor is multiple, multiple combined type acting rotor can share a firing chamber and also can not share a firing chamber and can also selectively divide into groups combustion chamber shared, the acting rotor shaft of described combined type acting rotor and rotor shaft of calming the anger can be the coaxial connections on same shaft axis also can be that the split axle carried out through planetary gear set on same shaft axis is connected, described rotor chamber of calming the anger can be can be cylindrical shape can also be able to not be also gradually put shape in convergence shape in convergence shape, described acting rotor chamber can also be able to be convergence shape in gradually to put shape can be cylindrical shape, described rotor air outlet of calming the anger there is gas storage valve connect with the outer caisson of body, described caisson can be applicable to the various of this programme in prior art can the gas storage equipment of storing compressed air, described gas storage valve can make rotor air outlet of calming the anger, firing chamber rear chamber and caisson three intercommunication, gas storage valve can also cut out rotor air outlet of calming the anger makes caisson communicate with firing chamber rear chamber separately, gas storage valve can also cut out the caisson rotor air outlet that makes to calm the anger and communicate separately with firing chamber rear chamber, combined type acting rotor main in described firing chamber front chamber, can there be flameholder at extra-air inlet place, described flameholder can be porous bell also can be that other can make gas flow rate in flameholder lower than the outer gas flow rate of flameholder by the more stable flameholder that can be used for the arbitrary shape of this programme of the burning of inflammable mixture, can there be rotatable cam axle at the described combined type acting enterprising gas port place of rotor non-turbine-type impeller cavity, non-turbine-type impeller cavity suction port can be closed or open to described camshaft, the aperture size of suction port can also be regulated and the gas flow simultaneously adjusted through suction port and direction by camshaft, it also can be communicated with toward the clockwise direction that described primary air inlet can counterclockwise be communicated with above upper semi-circle with non-turbine-type impeller cavity, that is calm the anger rotor and acting rotor can be rotated counterclockwise also can be dextrorotation rotatably, the bypass gas port place that chamber, described whirlpool follows air to communicate can only flow to and can not flow out outward when having bypass one-way valve to make extra-organismal air produce negative pressure in chamber, whirlpool in chamber, whirlpool, the outer secondary air outlet flue of gas port that described combined type acting rotor non-turbine-type impeller cavity air outlet follows return-air road to communicate there is outlet valve, secondary air outlet flue is communicated with main exhaust by outlet valve, described outlet valve can regulate and control and close secondary air outlet flue completely, described combined type acting rotor main, bypass valve on master air suction valve on extra-air inlet and secondary suction valve and chamber, whirlpool bypass air flue also has the return-air valve in return-air road to cut out completely and to open, described spring bearing can be the sealing support device with sealing and support function, as the shell type bearing with seal ring, watt formula bearing, also can be the needle bearing of band oil sealing, roller bearing, ball bearing, also can be magnetic suspension bearing, oil suspension bearing, it can also be the bearing of the form of ownership being applicable to this programme in prior art, described seal ring can be oil sealing, oil seal ring can also be the seal ring that can be used for this programme in prior art, described gas storage valve, gas-separating valve, master air suction valve, secondary suction valve, outlet valve, return-air valve, bypass valve on by-pass, one-way valve, fuel injector, secondary fuel injector, piston position controller and planetary gear set control gear, ignition mechanism, fuel supplying device can be all can be used for the electric controller of this programme or electric control mechanism and automatically controlled device in prior art.

The beneficial effect of this programme can be learnt according to describing of such scheme, due in this scenario one: at combined type acting rotor with calm the anger and connects acting rotor shaft by planetary gear set between rotor and calm the anger rotor shaft, because planetary gear set is a kind of special gear structure, the changeable easy control of its structural type can also choice structure pattern make combined type acting rotor and calm the anger between rotor automatically to adjust rotating ratio according to various working condition at work arbitrarily, combined type is allowed to do work rotor and calm the anger between rotor and accomplish self adaption, the rotating ratio that can also carry out adjustment combined type acting rotor by planetary gear set control gear and calm the anger between rotor, the rotor that makes to calm the anger can export the pressurized air of different compression ratio under same compound formula acting rotor speed condition, realize the variable adjustable controlled of compression ratio, the pressurized air of the different compression ratios required for multifuel firing can be provided to firing chamber under the condition not changing machine hardware, realize a machine multi fuel optional, acting rotor shaft is directly exported most of energy that combustion gas produces on primary and secondary acting turbine by the Gear combination of planetary gear set or other form, power turbine to squeeze in combustion gas remaining energy step by step and passes to charging turbine through supercharging rotor shaft and be used for acting of calming the anger, the energy that combustion gas produces obtains maximum utilization, improve fuel utilization efficiency.Two: in firing chamber, have the piston matched with circular diameter in firing chamber, in work, piston can according to automatically regulating relative position residing between chamber before and after in firing chamber under the assistance of different operating condition at spring at compressed air pressure forward and gaseous-pressure backward, can also be advanced by piston position controller and retract piston and piston position is adjusted, as: when use hydrogen, liquid gas, rock gas, during the gaseous fuels such as coal gas, due to the diffusivity of gaseous fuel, flammability is all relatively the highest, the front position that piston is pushed into forward firing chamber front chamber can be promoted with piston position controller, make firing chamber front chamber inner capacities relatively little, when use gasoline, light kerosene, during the volatile liquid fuel such as alcohol, due to the diffusivity of this class A fuel A, flammability is higher, piston can be pulled piston to be adjusted back to relative middle section position before and after in firing chamber between chamber with piston position controller, when use kerosene, during the not volatile heavy class A fuel A such as diesel oil, piston can be pulled piston to be adjusted back in firing chamber in rear chamber position more rearward with piston position controller, make firing chamber front chamber length relatively long, extend fuel from injection, be mixed into the distance of burning, relative prolongation fuel is done time in advance with compressed-air actuated, also have, pressurized air in the rear chamber of firing chamber is when fumarole sprays into firing chamber front chamber, under the guide functions of pressurized air guiding piece and guiding groove in fumarole by several angle helically eddy current spray into firing chamber front chamber, extend fuel relatively further from injection, be mixed into the distance of burning, extend fuel relatively further and improve mixture homogeneity diffusion time, make fuel combustion more abundant.Realize firing chamber variable adjustable controlled fuel Applicable scope is become wider.Three: the blade of the non-turbine-type impeller of combined type acting rotor has the tongue piece that can slide up and down, described tongue piece is at outside acting force of the spring, automatically can carry out regulating the relative position slided on blade according to different operating mode under the interaction of centrifugal force and inside acting gaseous-pressure, namely under identical gaseous-pressure can according to operating mode automatically regulate combined type do work rotor non-turbine-type impeller week/air displacement, also have, in work tongue piece slide up and down while by the circular arc air inlet duct on combined type acting rotor non-turbine-type impeller cavity sidewall again come from rotor of calming the anger or ozone that the temperature of air is lower pump into rotor cavity and pumped by outgassing groove again, reach the object making the cooling of combined type acting rotor.Four: the fumarole aperture that can be adjusted inner carrier center, firing chamber as required by fuel injector, regulate compression gas blowout flow of the people, realize fuel, pressurized gas is two-way adjustable, the bell flameholder of porous can make part inflammable mixture flow velocity low relative to the outer inflammable mixture flow velocity of flameholder, make combustion gas can smooth combustion under high flow rate, by the gas flow rate at camshaft adjustable combined type acting rotor non-turbine-type impeller suction port place and gas flow and direction.Five: when starting the machine, gas storage control valve is closed rotor air outlet of calming the anger and is opened caisson, caisson compressed air enters firing chamber front chamber through firing chamber rear chamber and opens with closing caisson after fuel mix ignition startup combined type acting rotor turns rotor suction port of calming the anger, what startup was become is simple, reliable, easy to operate, gas storage control valve can also be opened caisson as required and to be used for calming the anger in storage work the excess compressed air that rotor produces, need extra afterburning time discharge again to use and reach energy-conservation object.Six: combined type acting rotor main suction port and return-air road in work, can be closed completely, making high-pressure gas all enter chamber, whirlpool through combined type acting rotor extra-air inlet drives turbine-type page wheel to make combined type acting rotor rotate acting, waste gas is discharged through main exhaust, enter turbine engine mode of operation completely, also combined type acting rotor extra-air inlet and return-air road can be closed completely, high-pressure gas is entered in combined type acting rotor non-turbine-type impeller cavity through primary air inlet completely drives non-turbine-type impeller to make combined type acting rotor rotate acting, waste gas is discharged through secondary air outlet flue, enter non-turbine engine mode of operation completely, secondary air outlet flue can also be closed and open return-air road, the combustion gas cooled via return air road also after being done work in non-turbine-type impeller cavity air outlet place with certain pressure enters chamber, whirlpool and again drives turbine-type page to take turns rotation, waste gas is discharged through main exhaust, enter Combined-operating mode, the major-minor inlet close return-air road of combined type acting rotor can also be opened in right amount, make a high-pressure gas part enter chamber, whirlpool through extra-air inlet to drive turbine-type page to take turns another part to enter non-turbine-type impeller cavity through primary air inlet and drive non-turbine-type impeller, waste gas is discharged through major-minor air outlet flue respectively, enter blend modes of operation, accomplish that a machine multi-operation mode is optional.Seven: can open in work bypass valve allow the Partial shrinkage air from rotor of calming the anger enter chamber, whirlpool improve burning situation reduce exhaust emission, not only body outer air can be allowed in non-turbine-type mode of operation to enter chamber, whirlpool discharge through main exhaust again, to remove in chamber, whirlpool vacuum resistance but also serve to the object of combined type acting rotor cooling.In sum, the technical program has higher adaptive response and wider modification scope and simple to operationly also can realize the optional of multi fuel multi-operation mode under complex working conditions, because the rotor that done work by power stage is preposition, can the power turbine of rotor of calming the anger of multistage independent operation rearmounted, be equivalent to the turbosupercharger of having installed a set of multistage independent operation on turboshaft engine, combustion gas energy after acting is obtained absorb fully, its fuel utilization efficiency is higher, the operation of full electronic control technology can be realized, superiority due to its volume/power ratio is particularly suitable for the exploitation of the hybrid platform of computer programming intelligent control system.As can be seen here, the technical program compared with prior art, has novelty, substantive distinguishing features and remarkable progress, and its beneficial effect implemented also is apparent.

accompanying drawing illustrates:

Fig. 1 is the structural representation of this programme first embodiment.

Fig. 2 is along A place line cross cut structure schematic diagram in Fig. 1.

Fig. 3 is along B place line cross cut structure schematic diagram in Fig. 1.

Fig. 4 is along C place line cross cut structure schematic diagram in Fig. 1.

Fig. 5 is Fig. 1, Fig. 6, Figure 10, Figure 14, Figure 19, middle D place structure for amplifying schematic diagram.

Fig. 6 is the structural representation of this programme second embodiment.

Fig. 7 is along A place line cross cut structure schematic diagram in Fig. 6.

Fig. 8 is along B place line cross cut structure schematic diagram in Fig. 6.

Fig. 9 is along C place line cross cut structure schematic diagram in Fig. 6.

Figure 10 is the structural representation of this programme the 3rd embodiment.

Figure 11 is along A place line cross cut structure schematic diagram in Figure 10.

Figure 12 is along B place line cross cut structure schematic diagram in Figure 10.

Figure 13 is along C place line cross cut structure schematic diagram in Figure 10.

Figure 14 is the structural representation of this programme the 4th embodiment.

Figure 15 is along A place line cross cut structure schematic diagram in Figure 14.

Figure 16 is along B place line cross cut structure schematic diagram in Figure 14.

Figure 17 is along C place line cross cut structure schematic diagram in Figure 14, Figure 19.

Figure 18 is along E place line cross cut structure schematic diagram in Figure 14.

Figure 19 is the structural representation of this programme the 5th embodiment.

Figure 20 is along A place line cross cut structure schematic diagram in Figure 19.

Figure 21 is along B place line cross cut structure schematic diagram in Figure 19.

Figure 22 is along E place line cross cut structure schematic diagram in Figure 19.

Figure 23 is along F place line cross cut structure schematic diagram in Figure 19.

In figure, 1 is body, 2 is centrifugal compressor turbine, 3 is rotor shaft of calming the anger, 4 is wheel body, 5 is turbine-type turbine, 6 is non-turbine-type impeller, 7 is acting rotor shaft, 8 is rotor suction port of calming the anger, 9 is chamber, bowl-type whirlpool, 10 is planetary gear set, 11 is planetary gear set control gear, 12 is bypass air flue, 13 is bypass valve, 14 is air throttle, 15 is rotor air outlet of calming the anger, 16 is bypass one-way valve, 17 is gas-separating valve, 18 is non-turbine-type impeller blade, 19 is bearing, 20 is main exhaust, 21 is return-air road, 22 is return-air valve, 23 is cylindrical piston, 24 is piston ring, 25 is firing chamber front chamber, 26 is firing chamber rear chamber, 27 is fumarole, 28 is fuel injector, 29 is guiding piece, 30 is spring, 31 is piston position controller, 32 is telescopic pipe, 33 is fuel supplying device, 34 is gas storage valve, 35 is caisson, 36 is acting rotor main suction port, 37 is acting rotor extra-air inlet, 38 is ignition mechanism, 39 is flameholder, 40 is master air suction valve, 41 is secondary suction valve, 42 is camshaft, 43 is rotor cavity, 44 is acting rotor air outlet, 45 is secondary air outlet flue, 46 is secondary outlet valve, 47 is air inlet duct, 48 is air inlet duct one-way valve, 49 is outgassing groove, 50 is outgassing groove one-way valve, 51 is tongue piece, 52 is vent, 53 is hollow spacer dish, 54 is guiding piece, 55 is movable axis, 56 is tongue piece spring, 57 is wheel sheet, 58 is charging turbine, 58 ' is the second charging turbine, 58 〞 are the 3rd charging turbine, 59 is power turbine, 59 ' is the second power turbine, 59 〞 are the 3rd power turbine, 60 is power output shaft, 61 is basin tooth, 62 is cone tooth, 63 is supercharging rotor shaft, 63 ' is the second supercharging rotor shaft, 63 〞 are the 3rd supercharging rotor shaft.

embodiment:

For the technical characterstic of this programme more can be clearly demonstrated, below by five embodiments, and in conjunction with its accompanying drawing, this programme is further elaborated.

Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5 collectively illustrates this programme first embodiment, can be found out by accompanying drawing, internal-combustion engine shown in the present embodiment is by body 1 and charging turbine 58, what centrifugal compressor turbine 2 was formed calm the anger rotor and by wheel body 4, non-turbine-type impeller 6 also has power output shaft 60 with the combined type acting rotor of turbine-type turbine 5 formation and the acting rotor of power turbine 59 formation, basin tooth 61, cone tooth 62 is together formed, described charging turbine 58, what centrifugal compressor turbine 2 was formed calm the anger rotor and by wheel body 4, the combined type acting rotor that non-turbine-type impeller 6 is formed with turbine-type turbine 5 and the acting rotor that power turbine 59 is formed to be arranged on respectively in calm the anger rotor chamber and acting rotor chamber and with on an axis in body 1, described centrifugal compressor turbine 2 is contained in calms the anger on rotor shaft 3 front end, described wheel body 4 is arranged on acting rotor shaft 7 rear end, described turbine-type turbine 5 is arranged on wheel body 4, described non-turbine-type impeller 6 is arranged on the excircle of turbine-type turbine 5, described turbine-type turbine 5 has the chamber, bowl-type whirlpool 9 matched with turbine-type turbine 5 diameter above, described turbine-type turbine 5 has the guiding piece 54 matched with turbine-type turbine 5 hinge length below, described guiding piece 54 outer end is fixed on body 1, dynamic turbine 59 after described guiding piece 54, the length of blade of described power turbine 59 matches with guiding piece 54, described acting rotor shaft 7 front end passes forward from center, chamber, whirlpool 9 and connects with rotor shaft 3 rear end of calming the anger through planetary gear set 10, described planetary gear set 10 is through basin tooth 61, cone tooth 62 connects with power output shaft 60, described charging turbine 58 is arranged on supercharging rotor shaft 63 front end, described supercharging rotor shaft 63 rear end to be contained in rotor shaft 3 of calming the anger through centrifugal compressor turbine 2 central sleeve and to pass acting rotor shaft 7 rear end, described power turbine 59 is arranged on supercharging rotor shaft 63 rear end that passes through calm the anger rotor shaft 3 and acting rotor shaft 7 center, rotor suction port 8 of calming the anger before described body 1 communicates with charging turbine 58, guiding piece 54 is had with between charging turbine 58 at centrifugal compressor turbine 2, described guiding piece 54 angle of yaw is with adjacent centrifugal compressor turbine 2, charging turbine 58, turbine-type turbine 5, the hinge angle of yaw of power turbine 59 is contrary, described guiding piece 54 length is fixed on body 1 with charging turbine 58 hinge its outer end that matches, chamber 9, described bowl-type whirlpool is through turbine-type turbine 5, guiding piece 54, power turbine 59 communicates with main exhaust 20, described planetary gear set 10 there is planetary gear set control gear 11, chamber, described whirlpool 9 there is bypass air flue 12 communicate with the air outlet 15 of rotor of calming the anger and air, described bypass air flue 12 there is bypass valve 13, described bypass air flue 12 connects through the air outlet 15 of bypass valve 13 with rotor of calming the anger, described bypass air flue 12 has bypass one-way valve 16 on the outer gas port communicated with air of bypass valve 13, secondary fuel injector 28 ' is had on described bypass valve 13 internal bypass air flue 12 He on secondary intake duct 37, described secondary fuel injector 28 ' is communicated with fuel supplying device 33, described non-turbine-type impeller 6 is unshrouded impeller structures, with the contact of chamber wall on the excircle that described non-turbine-type impeller 6 upper blade 18 is fixed on turbine-type turbine 5, described non-turbine-type impeller 6 chamber lower semi-circle has air outlet 44 on the sidewall of side, chamber, whirlpool 9, described air outlet 44 there is return-air road 21, described return-air road 21 communicates with chamber, whirlpool 9, there is bearing 19 to be contained in described body 1 spacing wall and calm the anger on rotor shaft 3 and acting rotor shaft 7, above described combined type acting rotor, body 1 there is throat less chamber, there is the cylindrical piston 23 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 23 periphery there is sealed piston ring 24, described cylindrical piston 23 is divided into front chamber 25 and rear chamber 26 firing chamber, cylindrical piston 23 can in the front chamber 25 of firing chamber and rear chamber 26 slide anteroposterior, there is fumarole 27 at described piston 23 center, described fumarole 27 center be equipped with can antero posterior axis to the fuel injector 28 of activity, described fumarole 27 there is guiding piece 29, spring 30 is had in described cylindrical piston 23 rear end firing chamber rear chamber 26, piston position controller 31 is had in described spring 30 rear end firing chamber rear chamber 26, telescopic pipe 32 is had in described rear chamber 26 li of springs 30 enclose, described telescopic pipe 32 front end is communicated with fuel injector 28, its rear end is through piston position controller 31, body 1 is communicated with fuel supplying device 33, described firing chamber rear chamber 26 rear end communicates with rotor air outlet 15 of calming the anger, described rotor air outlet 15 of calming the anger there is gas storage valve 34, described gas storage valve 34 communicates with the outer caisson 35 of body 1, described firing chamber front chamber 25 front end is communicated with extra-air inlet 37 with combined type acting rotor main suction port 36, above combined type acting rotor main suction port 36 and extra-air inlet 37, ignition mechanism 38 and flameholder 39 are installed in described firing chamber front chamber 25 front end, described primary air inlet 36 is counterclockwise communicated with above upper semi-circle with non-turbine-type impeller 6 chamber, described extra-air inlet 37 is communicated with chamber, turbine-type turbine 5 front whirlpool 9, there is gas-separating valve 17 in the intersection of described combined type acting rotor main suction port 36 and extra-air inlet 37, in described primary air inlet 36, non-turbine-type impeller 6 chamber there is rotatable cam axle 42, described rotor shaft 3 of calming the anger is followed between supercharging rotor shaft 63 and acting rotor shaft 7 has spring bearing 19 with between supercharging rotor shaft 63.

Fig. 5, Fig. 6, Fig. 7, Fig. 8, Fig. 9 shows this programme second embodiment, can be found out by accompanying drawing, internal-combustion engine shown in the present embodiment is by body 1, rotor of calming the anger is formed with acting rotor, described rotor of calming the anger same axis is arranged on respectively in body 1 with acting rotor calms the anger in rotor chamber and acting rotor chamber, described rotor of calming the anger is by centrifugal compressor turbine 2, charging turbine 58, second charging turbine 58 ' is formed, described acting rotor follows power turbine 59 by hybrid rotor rotor, second power turbine 59 ' is formed, described combined type acting rotor is by wheel body 4, turbine-type turbine 5 and non-turbine-type impeller 6 are formed, described centrifugal compressor turbine 2 is arranged on calms the anger on rotor shaft 3 front end, described wheel body 4 is arranged on acting rotor shaft 7 rear end, described turbine-type turbine 5 is arranged on wheel body 4, described non-turbine-type impeller 6 is arranged on the excircle of turbine-type turbine 5, described turbine-type turbine 5 has the chamber, bowl-type whirlpool 9 matched with turbine-type turbine 5 diameter above, described acting rotor shaft 7 front end passes from Wo Qiang 9 bottom centre and connects with rotor shaft 3 rear end of calming the anger through planetary gear set 10, described planetary gear set 10 there is planetary gear set control gear 11, described acting rotor shaft 7 is through planetary gear set 10, basin tooth 61, cone tooth 62 connects with power output shaft 60, described charging turbine 58 is installed on supercharging rotor shaft 63 front end, described supercharging rotor shaft 63 rear end is passed centrifugal compressor turbine 2 center and is sleeved in rotor shaft 3 of calming the anger and passes acting rotor shaft 7 rear end and install power turbine 59, described second charging turbine 58 ' is arranged on the second supercharging rotor shaft 63 ' front end, described second supercharging rotor shaft 63 ' to be contained in supercharging rotor shaft 63 through charging turbine 58 central sleeve and to pass supercharging rotor shaft 63 rear end installs the second power turbine 59 ', at centrifugal compressor turbine 2 with between charging turbine 58, charging turbine 58 is followed between the second charging turbine 58 ' and at turbine-type turbine 5 with between power turbine 59, power turbine 59 has guiding piece 54 with between the second power turbine 59 ', guiding piece 54 angle of yaw is with adjacent centrifugal compressor turbine 2, charging turbine 58, second charging turbine 58 ', turbine-type turbine 5, power turbine 59, the hinge angle of yaw of the second power turbine 59 ' is contrary, described body 1 has suction port 8 to communicate with the second charging turbine 58 ' above, described second power turbine 59 ' has the main exhaust 20 matched with the second power turbine 59 ' diameter below, chamber 9, described bowl-type whirlpool is through turbine-type turbine 5, guiding piece 54, power turbine 59, second power turbine 59 ' communicates with main exhaust 20, described rotor shaft 3 of calming the anger is with between supercharging rotor shaft 63, acting rotor shaft 7 has spring bearing 19 with between supercharging rotor shaft 63 and at supercharging rotor shaft 63 with between the second supercharging rotor shaft 63 ', chamber, described whirlpool 9 there is bypass air flue 12 communicate with calm the anger rotor air outlet 15 and air, air throttle 14 is had in the air flue that described bypass air flue 12 communicates with rotor air outlet 15 of calming the anger, the gas port that described bypass air flue 12 follows air to communicate there is bypass one-way valve 16, described bypass air flue 12 there is secondary fuel injector 28 ' after air throttle 14, described secondary fuel injector 28 ' is communicated with fuel supplying device 33, described non-turbine-type impeller 6 is unshrouded impeller structures, with the contact of chamber wall on the excircle that described non-turbine-type impeller 6 blade 18 is fixed on turbine-type turbine 5, described non-turbine-type impeller 6 chamber lower semi-circle circumferentially has air outlet 44, described air outlet 44 there is return-air road 21, described air outlet 44 air flue last time 21 mouthfuls has secondary air outlet flue 45 outward, described return-air road 21 communicates with chamber, whirlpool 9, described return-air road 21 there is return-air valve 22, the outer secondary air outlet flue 45 of described air outlet 44 air flue last time 21 mouthfuls there is outlet valve 46, sealing is had in described body 1 spacing wall, the bearing 19 of support function is contained in calms the anger on rotor shaft 3 and acting rotor shaft 7, above described combined type acting rotor chamber, body 1 there is throat less chamber, there is the cylindrical piston 23 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 23 periphery there is sealed piston ring 24, described cylindrical piston 23 is divided into front chamber 25 and rear chamber 26 firing chamber, cylindrical piston 23 can in the front chamber 25 of firing chamber and rear chamber 26 slide anteroposterior, there is fumarole 27 at described piston 23 center, described fumarole 27 center be equipped with can antero posterior axis to the fuel injector 28 of activity, described fumarole 27 there is spirally-guided sheet 29, spring 30 is had in described cylindrical piston 23 rear end firing chamber rear chamber 26, piston position controller 31 is had in described spring 30 rear end firing chamber rear chamber 26, described rear chamber 26 inner spring 30 has telescopic pipe 32 in enclosing, described telescopic pipe 32 front end is communicated with fuel injector 28, described telescopic pipe 32 rear end is through piston position controller 31, body 1 is communicated with fuel supplying device 33, described firing chamber rear chamber 26 rear end communicates with rotor air outlet 15 of calming the anger, described rotor air outlet 15 of calming the anger there is gas storage valve 34, described gas storage valve 34 communicates with the outer caisson 35 of body 1, described firing chamber front chamber 25 front end is communicated with extra-air inlet 37 with combined type acting rotor main suction port 36, in described firing chamber front chamber 25 front end, combined type acting rotor main suction port 36 and extra-air inlet 37 are provided with ignition mechanism 38 and flameholder 39, described primary air inlet 36 is counterclockwise communicated with above upper semi-circle with non-turbine-type impeller 6 chamber, described extra-air inlet 37 is communicated with chamber, turbine-type turbine 5 front whirlpool 9, secondary fuel injector 28 ' is had in described extra-air inlet 37, described secondary fuel injector 28 ' is communicated with fuel supplying device 33, described combined type acting rotor main suction port 36 there is master air suction valve 40, described extra-air inlet 37 there is secondary suction valve 41, rotatable cam axle 42 is had above non-turbine-type impeller 6 chamber after master air suction valve 40 in described primary air inlet 36.

Fig. 5, Figure 10, Figure 11, Figure 12, Figure 13 shows this programme the 3rd embodiment, can be found out by accompanying drawing, internal-combustion engine shown in the present embodiment is by body 1, rotor of calming the anger is formed with acting rotor, described rotor of calming the anger same axis is arranged on respectively in body 1 with acting rotor calms the anger in rotor chamber and acting rotor chamber, described rotor of calming the anger is by centrifugal compressor turbine 2, charging turbine 58, second charging turbine 58 ', 3rd charging turbine 58 〞 is formed, described acting rotor is by combined type acting rotor and power turbine 59, second power turbine 59 ', 3rd power turbine 59 〞 is formed, described combined type acting rotor is by wheel body 4, turbine-type turbine 5, non-turbine-type impeller 6 is formed, described centrifugal compressor turbine 2 is arranged on calms the anger on rotor shaft 3 front end, described acting rotor shaft 7 rear end is provided with wheel body 4 and the second wheel body 4 ' successively, described turbine-type turbine 5 is arranged on wheel body 4, described second turbine-type turbine 5 ' is arranged on the second wheel body 4 ', described non-turbine-type impeller 6 is arranged on the excircle of turbine-type turbine 5, described turbine-type turbine 5 has the chamber, bowl-type whirlpool 9 matched with turbine-type turbine 5 diameter above, described acting rotor shaft 7 front end passes from Wo Qiang 9 bottom centre and connects with rotor shaft 3 of calming the anger through planetary gear set 10, described planetary gear set 10 there is planetary gear set control gear 11, described acting rotor shaft 7 is through planetary gear set 10, basin tooth 61, cone tooth 62 connects with power output shaft 60, described charging turbine 58 is arranged on supercharging rotor shaft 63 front end, described supercharging rotor shaft 63 rear end to be contained in rotor shaft 3 of calming the anger through centrifugal compressor turbine 2 central sleeve and to pass acting rotor shaft 7 rear end installs power turbine 59, described second charging turbine 58 ' is arranged on the second supercharging rotor shaft 63 ' front end, described second supercharging rotor shaft 63 ' rear end to be contained in supercharging rotor shaft 63 through charging turbine 58 central sleeve and to pass supercharging rotor shaft 63 rear end installs the second power turbine 59, described 3rd charging turbine 58 〞 is arranged on the 3rd supercharging rotor shaft 63 〞 front end, described 3rd supercharging rotor shaft 63 〞 rear end to be contained in the second supercharging rotor shaft 63 ' cylinder through the second charging turbine 58 ' central sleeve and to pass the second supercharging rotor shaft 63 ' rear end installs the 3rd power turbine 59 〞, described body 1 has suction port 8 to communicate with the 3rd charging turbine 58 〞 above, the main exhaust 20 matched with the 3rd power turbine 59 〞 diameter is had after described 3rd power turbine 59 〞, described centrifugal compressor turbine 2 is with between charging turbine 58, charging turbine 58 is with between the second charging turbine 58 ', second charging turbine 58 ' has guiding piece 54 with between the 3rd charging turbine 58 〞, described guiding piece 54 outer end is fixed on body 1, described turbine-type turbine 5 is with between the second turbine-type turbine 5 ', second turbine-type turbine 5 ' is with between power turbine 59, power turbine 59 is with between the second power turbine 59 ', second power turbine 59 ' has hollow spacer dish 53 and guiding piece 54 with between the 3rd power turbine 59 〞, described guiding piece 54 outer end is fixed on body 1, its the inner is fixed on space disc 53, described guiding piece 54 angle of yaw is with centrifugal compressor turbine 2, charging turbine 58, second charging turbine 58 ', 3rd charging turbine 58 〞, turbine-type turbine 5, second turbine-type turbine 5 ', power turbine 59, second power turbine 59 ', hinge angle of yaw on 3rd power turbine 59 〞 is contrary, described rotor shaft 3 of calming the anger is with between supercharging rotor shaft 63, acting rotor shaft 7 is with between supercharging rotor shaft 63, supercharging rotor shaft 63 is with between the second supercharging rotor shaft 63 ', second supercharging rotor shaft 63 ' has sealing with between the 3rd supercharging rotor shaft 63 〞, the spring bearing 19 of support function, chamber, described whirlpool 9 there is bypass air flue 12 communicate with calm the anger rotor and air, air throttle 14 is had in the air flue that described bypass air flue 12 communicates with rotor of calming the anger, described bypass air flue 12 connects with rotor air outlet 15 of calming the anger, the gas port that described bypass air flue 12 follows air to communicate there is bypass one-way valve 16, described air throttle 14 internal bypass air flue 12 there is secondary fuel injector 28 ', described fuel injector 28 ' is communicated with fuel supplying device 33, described non-turbine-type impeller 6 is unshrouded impeller structures, described non-turbine-type impeller 6 upper blade 18 tilts counterclockwise and is fixed on the excircle of turbine-type turbine 5 not with the contact of chamber wall, described non-turbine-type impeller 6 chamber lower semi-circle circumferentially has air outlet 44, described air outlet 44 there is return-air road 21, described air outlet 44 air flue last time 21 mouthfuls has secondary air outlet flue 45 outward, described return-air road 21 communicates with chamber, whirlpool 9, described return-air road 21 there is return-air valve 22, the outer secondary air outlet flue 45 of described air outlet 44 air flue last time 21 mouthfuls there is outlet valve 46, spring bearing 19 is had to be contained in rotor shaft 3 of calming the anger in described body 1 spacing wall, on acting rotor shaft 7, above described combined type acting rotor, body 1 there is throat less chamber, there is the cylindrical piston 23 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 23 periphery there is sealed piston ring 24, described cylindrical piston 23 is divided into front chamber 25 and rear chamber 26 firing chamber, cylindrical piston 23 can in the front chamber 25 of firing chamber and rear chamber 26 slide anteroposterior, there is fumarole 27 at described piston 23 center, described fumarole 27 center be equipped with can antero posterior axis to the fuel injector 28 of activity, described fumarole 27 there is guiding piece 29, piston position controller 31 is had in described cylindrical piston 23 rear end firing chamber rear chamber 26, telescopic pipe 32 is had in described firing chamber rear chamber 26, described telescopic pipe 32 front end is communicated with fuel injector 28, rear end is through piston position controller 31, body 1 is communicated with fuel supplying device 33, described firing chamber rear chamber 26 rear end communicates with rotor air outlet 15 of calming the anger, described rotor air outlet 15 of calming the anger there is gas storage valve 34, described gas storage valve 34 communicates with the outer caisson 35 of body 1, described firing chamber front chamber 25 front end is communicated with extra-air inlet 37 with combined type acting rotor main suction port 36, above combined type acting rotor main suction port 36 and extra-air inlet 37, ignition mechanism 38 and flameholder 39 are installed in described firing chamber front chamber 25 front end, described primary air inlet 36 is counterclockwise communicated with above upper semi-circle with non-turbine-type impeller 6 chamber, described extra-air inlet 37 is communicated with chamber, turbine-type turbine 5 front whirlpool 9, described combined type acting rotor main suction port 36 there is master air suction valve 40, described extra-air inlet 37 there is secondary suction valve 41, rotatable cam axle 42 is had above non-turbine-type impeller 6 chamber after master air suction valve 40 in described primary air inlet 36, described extra-air inlet 37 there is secondary fuel injector 28 ', described fuel injector 28 ' is communicated with fuel supplying device 33, chamber 9, described bowl-type whirlpool is through turbine-type turbine 5, second turbine-type turbine 5 ', power turbine 59, second power turbine 59 ', 3rd power turbine 59 〞 is communicated with the main exhaust 20 after the 3rd power turbine 59 〞.

Fig. 5, Figure 14, Figure 15, Figure 16, Figure 17, Figure 18 shows this programme the 4th embodiment, internal-combustion engine shown in the present embodiment is by body 1 and charging turbine 58, what centrifugal compressor turbine 2 was formed calm the anger rotor and by wheel body 4, non-turbine-type impeller 6 also has power output shaft 60 with the combined type acting rotor of turbine-type turbine 5 formation and the acting rotor of power turbine 59 formation, basin tooth 61, cone tooth 62 is together formed, described charging turbine 58, what centrifugal compressor turbine 2 was formed calm the anger rotor and by wheel body 4, the combined type acting rotor that non-turbine-type impeller 6 is formed with turbine-type turbine 5 and the acting rotor that power turbine 59 is formed to be arranged on respectively in calm the anger rotor chamber and acting rotor chamber and with on an axis in body 1, described centrifugal compressor turbine 2 is contained in calms the anger on rotor shaft 3 front end, described wheel body 4 is arranged on acting rotor shaft 7 rear end, described turbine-type turbine 5 is arranged on wheel body 4, described non-turbine-type impeller 6 is arranged on the excircle of turbine-type turbine 5, described turbine-type turbine 5 has the chamber, bowl-type whirlpool 9 matched with turbine-type turbine 5 diameter above, described turbine-type turbine 5 has the guiding piece 54 matched with turbine-type turbine 5 hinge length below, described guiding piece 54 outer end is fixed on body 1, dynamic turbine 59 after described guiding piece 54, the length of blade of described power turbine 59 matches with guiding piece 54, described acting rotor shaft 7 front end passes forward from center, chamber, whirlpool 9 and connects with rotor shaft 3 rear end of calming the anger through planetary gear set 10, described planetary gear set 10 there is planetary gear set control gear 11, described planetary gear set 10 is through basin tooth 61, cone tooth 62 connects with power output shaft 60, described charging turbine 58 is arranged on supercharging rotor shaft 63 front end, described supercharging rotor shaft 63 rear end to be contained in rotor shaft 3 of calming the anger through centrifugal compressor turbine 2 central sleeve and to pass acting rotor shaft 7 rear end, described power turbine 59 is arranged on supercharging rotor shaft 63 rear end that passes through calm the anger rotor shaft 3 and acting rotor shaft 7 center, guiding piece 54 is had with between charging turbine 58 at centrifugal compressor turbine 2, described guiding piece 54 length is fixed on body 1 with charging turbine 58 hinge its outer end that matches, described guiding piece 54 angle of yaw is with adjacent centrifugal compressor turbine 2, charging turbine 58, turbine-type turbine 5, hinge angle of yaw on power turbine 59 is contrary, described body 1 has suction port 8 to communicate with charging turbine 58 above, chamber 9, described bowl-type whirlpool is through turbine-type turbine 5, guiding piece 54, power turbine 59 communicates with main exhaust 20, described rotor shaft 3 of calming the anger is followed between supercharging rotor shaft 63 and acting rotor shaft 7 has spring bearing 19 with between supercharging rotor shaft 63, chamber, described whirlpool 9 there is bypass air flue 12 communicate with calm the anger rotor and air, described bypass air flue 12 there is bypass valve 13, described bypass air flue 12 there is air throttle 14 in the outer air flue communicated with rotor of calming the anger of bypass valve 13, described bypass air flue 12 is through bypass valve 13, air throttle 14 connects with rotor air outlet 15 of calming the anger, the outer gas port of following air to communicate of bypass valve 13 there is bypass one-way valve 16 to described bypass air flue 12, described bypass air flue 12 there is secondary fuel injector 28 ', described secondary fuel injector 28 ' connects with fuel supplying device 33, described non-turbine-type impeller 6 is unshrouded impeller structures, with the contact of chamber wall on the excircle that described non-turbine-type impeller 6 upper blade 18 is fixed on turbine-type turbine 5, described combined type acting rotor non-turbine-type impeller 6 has with blade 18 with wide tongue piece 51 between adjacent two blades 18, a limit of described tongue piece 51 with left side blade 18 top margin in adjacent two blades 18 through the Viability connection of movable axis 55, the blade face that described tongue piece 51 is its another edge, axle center another blade 18 adjacent with movable axis 55 slides up and down in scope between zero to nine ten degree, its top dead center is no more than corresponding blade 18 top margin slided, the slip radian of 18 its radians of camber of the blade corresponding to described tongue piece 51 sliding edge and tongue piece 51 sliding edge matches, described tongue piece 51 active edges is adjacent two blades 18 when top dead center, tongue piece 51, the interior wheel between week and two side, non-turbine-type impeller 6 chamber at blade 18 place forms a rotor cavity 43, described rotor cavity 43 internal tongue 51 has tongue piece spring 56 below, inside the upper semi-circle of described combined type acting rotor non-turbine-type impeller 6 chamber, chamber wall internal circle have with circular arc outgassing groove 49 corresponding bottom rotor cavity 43 in primary air inlet 36 side below, described circular arc outgassing groove 49 front end communicates with the chamber, whirlpool 9 before combined type acting rotor turbine-type turbine 5, the gas port that described circular arc outgassing groove 49 follows chamber, whirlpool to communicate there is outgassing groove one-way valve 50, inside the lower semi-circle of described combined type acting rotor non-turbine-type impeller 6 chamber, chamber wall internal circle have with circular arc air inlet duct 47 corresponding bottom rotor cavity 43 in side, air outlet 44, described air inlet duct 47 is communicated with between bypass valve 13 and bypass one-way valve 16 and air throttle 14 on bypass air flue 12 through air flue, the gas port of described air inlet duct 47 with bypass air flue 12 connection there is air inlet duct one-way valve 48, communicate with corresponding circular arc outgassing groove 49 and circular arc air inlet duct 47 on the sidewall of combined type acting rotor non-turbine-type impeller 6 chamber bottom described rotor cavity 43, described non-turbine-type impeller 6 chamber lower semi-circle circumferentially has air outlet 44, described air outlet 44 there is return-air road 21, described air outlet 44 air flue last time 21 mouthfuls has secondary air outlet flue 45 outward, described return-air road 21 communicates with chamber, whirlpool 9, described return-air road 21 there is return-air valve 22, the outer secondary air outlet flue 45 of described air outlet 44 air flue last time 21 mouthfuls there is outlet valve 46, there is bearing 19 to be contained in described body 1 spacing wall and calm the anger on rotor shaft 3 and acting rotor shaft 7, above described combined type acting rotor, body 1 there is throat less chamber, there is the cylindrical piston 23 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 23 periphery there is sealed piston ring 24, described cylindrical piston 23 is divided into front chamber 25 and rear chamber 26 firing chamber, cylindrical piston 23 can in the front chamber 25 of firing chamber and rear chamber 26 slide anteroposterior, there is fumarole 27 at described piston 23 center, described fumarole 27 center be equipped with can antero posterior axis to the fuel injector 28 of activity, described fumarole 27 there is guiding piece 29, spring 30 is had in described cylindrical piston 23 rear end firing chamber rear chamber 26, piston position controller 31 is had in described spring 30 rear end firing chamber rear chamber 26, telescopic pipe 32 is had in described rear chamber 26 spring 30 encloses, described telescopic pipe 32 front end is communicated with fuel injector 28, rear end is through piston position controller 31, body 1 is communicated with fuel supplying device 33, described firing chamber rear chamber 26 rear end communicates with rotor air outlet 15 of calming the anger, described rotor air outlet 15 of calming the anger there is gas storage valve 34, described gas storage valve 34 communicates with the outer caisson 35 of body 1, described firing chamber front chamber 25 front end is communicated with extra-air inlet 37 with combined type acting rotor main suction port 36, above combined type acting rotor main suction port 36 and extra-air inlet 37, ignition mechanism 38 and flameholder 39 are installed in described firing chamber front chamber 25 front end, described primary air inlet 36 is counterclockwise communicated with above upper semi-circle with non-turbine-type impeller 6 chamber, described extra-air inlet 37 is communicated with chamber, turbine-type turbine 5 front whirlpool 9, described combined type acting rotor main suction port 36 there is master air suction valve 40, described extra-air inlet 37 there is secondary suction valve 41, rotatable cam axle 42 is had above non-turbine-type impeller 6 chamber after master air suction valve 40 in described primary air inlet 36.

Fig. 5, Figure 17, Figure 19, Figure 20, Figure 21, Figure 22, Figure 23 shows this programme the 5th embodiment, internal-combustion engine shown in the present embodiment is by body 1 and charging turbine 58, what centrifugal compressor turbine 2 was formed calm the anger rotor and by wheel body 4, second wheel body 4 ', non-turbine-type impeller 6 is with turbine-type turbine 5, the combined type acting rotor that second turbine-type turbine 5 ' is formed and the acting rotor that power turbine 59 is formed also have power output shaft 60, basin tooth 61, cone tooth 62 is together formed, described charging turbine 58, what centrifugal compressor turbine 2 was formed calm the anger rotor and by wheel body 4, second wheel body 4 ', non-turbine-type impeller 6 is with turbine-type turbine 5, the combined type acting rotor that second turbine-type turbine 5 ' is formed and the acting rotor that power turbine 59 is formed to be arranged on respectively in calm the anger rotor chamber and acting rotor chamber and with on an axis in body 1, described centrifugal compressor turbine 2 is contained in calms the anger on rotor shaft 3 front end, described wheel body 4 and the second wheel body 4 ' are arranged on acting rotor shaft 7 rear end successively, described turbine-type turbine 5 is arranged on wheel body 4, described second turbine-type turbine 5 ' is arranged on the second wheel body 4 ', described non-turbine-type impeller 6 is arranged on the excircle of the second turbine-type turbine 5 ', described turbine-type turbine 5 has the chamber, bowl-type whirlpool 9 matched with turbine-type turbine 5 diameter above, described turbine-type turbine 5 has the guiding piece 54 and hollow spacer dish 53 that match with turbine-type turbine 5 hinge length below, described guiding piece 54 outer end is fixed on the inner on body 1 and is fixed on the excircle of hollow spacer dish 53, it is the second turbine-type turbine 5 ' after described guiding piece 54, described acting rotor shaft 7 front end passes forward from Wo Qiang 9 bottom centre and connects with rotor shaft 3 rear end of calming the anger through planetary gear set 10, described planetary gear set 10 there is planetary gear set control gear 11, described planetary gear set 10 is through basin tooth 61, cone tooth 62 connects with power output shaft 60, described charging turbine 58 is arranged on supercharging rotor shaft 63 front end, described supercharging rotor shaft 63 rear end to be contained in rotor shaft 3 of calming the anger through centrifugal compressor turbine 2 central sleeve and to pass acting rotor shaft 7 rear end, described power turbine 59 is arranged on supercharging rotor shaft 63 rear end that passes through calm the anger rotor shaft 3 and acting rotor shaft 7 center, guiding piece 54 is had with between charging turbine 58 at centrifugal compressor turbine 2, at turbine-type turbine 5 with between the second turbine-type turbine 5 ', second turbine-type turbine 5 ' is with having guiding piece 54 and hollow spacer dish 53 between power turbine 59, the length of blade of described power turbine 59 matches with guiding piece 54, described guiding piece 54 outer end is fixed on the inner on body 1 and is fixed on the excircle of hollow spacer dish 53, described guiding piece 54 angle of yaw is with adjacent centrifugal compressor turbine 2, charging turbine 58, turbine-type turbine 5, second turbine-type turbine 5 ', hinge angle of yaw on power turbine 59 is contrary, described body 1 has suction port 8 to communicate with charging turbine 58 above, chamber 9, described bowl-type whirlpool is through turbine-type turbine 5, guiding piece 54, second turbine-type turbine 5 ', guiding piece 54, power turbine 59 communicates with main exhaust 20, described rotor shaft 3 of calming the anger is followed between supercharging rotor shaft 63 and acting rotor shaft 7 has spring bearing 19 with between supercharging rotor shaft 63, described turbine-type page wheel 5, second turbine-type turbine 5 ', hinge deflection direction on power turbine 59 and charging turbine 58 is identical, chamber, described whirlpool 9 there is bypass air flue 12 communicate with calm the anger rotor and air, described bypass air flue 12 there is bypass valve 13, described bypass air flue 12 there is air throttle 14 in the outer air flue communicated with rotor of calming the anger of bypass valve 13, described bypass air flue 12 is through bypass valve 13, air throttle 14 connects with the air outlet 15 of rotor of calming the anger, the outer gas port of following air to communicate of bypass valve 13 there is bypass one-way valve 16 to described bypass air flue 12, with the contact of chamber wall on the excircle that described non-turbine-type impeller 6 upper blade 18 is fixed on the second turbine-type turbine 5 ', described non-turbine-type impeller 6 upper blade 18 both sides are by the double shrouded wheel structure of taking turns sheet 57 shutoff, described combined type acting rotor non-turbine-type impeller 6 has with blade 18 with wide tongue piece 51 between adjacent two blades 18, a limit of described tongue piece 51 with right side blade 18 top margin in adjacent two blades 18 through the Viability connection of movable axis 55, the blade face that described tongue piece 51 is its another edge, axle center another blade 18 adjacent with movable axis 55 slides up and down in scope between zero to nine ten degree, its top dead center is no more than corresponding blade 18 top margin slided, the slip radian of blade 18 its radians of camber that described tongue piece 51 sliding edge is corresponding and tongue piece 51 sliding edge matches, described tongue piece 51 active edges is adjacent two blades 18 when top dead center, the wheel sheet 57 of blade 18 both sides, tongue piece 51, the interior wheel between week at blade 18 place forms a rotor cavity 43, inside the upper semi-circle of described combined type acting rotor non-turbine-type impeller 6 chamber, chamber wall internal circle have with circular arc outgassing groove 49 corresponding bottom rotor cavity 43 in primary air inlet 36 side, described circular arc outgassing groove 49 front end communicates with the chamber, whirlpool 9 before combined type acting rotor turbine-type turbine 5, the gas port that described circular arc outgassing groove 49 follows chamber, whirlpool to communicate there is outgassing groove one-way valve 50, described combined type acting lower semi-circle opposite side chamber, rotor non-turbine-type impeller 6 chamber wall internal circle have with circular arc air inlet duct 47 corresponding bottom rotor cavity 43 in side, air outlet 44, described air inlet duct 47 is communicated with between bypass valve 13 and bypass one-way valve 16 and air throttle 14 on bypass air flue 12 through air flue, the gas port of described air inlet duct 47 with bypass air flue 12 connection there is air inlet duct one-way valve 48, described rotor cavity 43 two bottom sides wheel sheet 57 there is the vent 52 communicated with corresponding circular arc outgassing groove 49 and circular arc air inlet duct 47 on the sidewall of combined type acting rotor non-turbine-type impeller 6 chamber, described non-turbine-type impeller 6 chamber lower semi-circle circumferentially has air outlet 44, described air outlet 44 there is return-air road 21, described air outlet 44 air flue last time 21 mouthfuls has secondary air outlet flue 45 outward, described return-air road 21 communicates with chamber, whirlpool 9, described return-air road 21 there is return-air valve 22, the outer secondary air outlet flue 45 of described air outlet 44 air flue last time 21 mouthfuls there is outlet valve 46, described bypass valve 13 internal bypass air flue 12 there is secondary fuel injector 28 ', described secondary fuel injector 28 ' connects with fuel supplying device 33, there is bearing 19 to be contained in described body 1 spacing wall and calm the anger on rotor shaft 3 and acting rotor shaft 7, described rotor shaft 3 of calming the anger is followed between supercharging rotor shaft 63 and acting rotor shaft 7 has spring bearing 19 with between supercharging rotor shaft 63, above described combined type acting rotor, body 1 there is throat less chamber, there is the cylindrical piston 23 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 23 periphery there is sealed piston ring 24, described cylindrical piston 23 is divided into front chamber 25 and rear chamber 26 firing chamber, cylindrical piston 23 can in the front chamber 25 of firing chamber and rear chamber 26 slide anteroposterior, there is fumarole 27 at described piston 23 center, described fumarole 27 center be equipped with can antero posterior axis to the fuel injector 28 of activity, described fumarole 27 there is guiding piece 29, spring 30 is had in described cylindrical piston 23 rear end firing chamber rear chamber 26, piston position controller 31 is had in described spring 30 rear end firing chamber rear chamber 26, telescopic pipe 32 is had in described rear chamber 26 spring 30 encloses, described telescopic pipe 32 front end is communicated with fuel injector 28, rear end is through piston position controller 31, body 1 is communicated with fuel supplying device 33, described firing chamber rear chamber 26 rear end communicates with rotor air outlet 15 of calming the anger, described rotor air outlet 15 of calming the anger there is gas storage valve 34, described gas storage valve 34 communicates with the outer caisson 35 of body 1, described firing chamber front chamber 25 front end is communicated with extra-air inlet 37 with combined type acting rotor main suction port 36, ignition mechanism 38 and flameholder 39 is had above combined type acting rotor main suction port 36 and extra-air inlet 37 in described firing chamber front chamber 25 front end, described primary air inlet 36 is counterclockwise communicated with above upper semi-circle with non-turbine-type impeller 6 chamber, described extra-air inlet 37 is communicated with chamber, turbine-type turbine 5 front whirlpool 9, described combined type acting rotor main suction port 36 there is master air suction valve 40, described extra-air inlet 37 there is secondary suction valve 41, in described secondary suction valve 41, secondary intake duct 37 there is secondary fuel injector 28 ', described secondary fuel injector 28 ' connects with fuel supplying device 33, rotatable cam axle 42 is had above non-turbine-type impeller 6 chamber after master air suction valve 40 in described primary air inlet 36.

Basic functional principle and advantage: first allow gas storage valve 34 close rotor air outlet 15 of calming the anger and open caisson 35, the pressurized air with certain pressure is entered in firing chamber rear chamber 26 through gas storage valve 34 and promotes piston 23 forward slip increasing fumarole 27 aperture, pressurized air spray into from fumarole 27 firing chamber front chamber 25 simultaneously fuel injector 28 spray fuel and be mixed to form inflammable mixture with pressurized air, an inflammable mixture part enters in flameholder 39 to be converged together by ignition mechanism 38 ignition combustion expansion generation high-temperature high-pressure fuel gas through flameholder 39 with the inflammable mixture flow through outside flameholder 39, high-temperature high-pressure fuel gas promotes piston 23 and reduces fumarole 27 aperture to rear chamber 26 sliding compression spring 30 and open return-air valve 22 on master air suction valve 40 and camshaft 42 on primary air inlet 36 and return-air road 21 and the bypass valve 13 on the secondary suction valve 41 of closing on extra-air inlet 37 and chamber, whirlpool 9 bypass air flue 12 and the outlet valve 46 on secondary air outlet flue 45 simultaneously, the master air suction valve 40 of high-temperature high-pressure fuel gas all on primary air inlet 36, camshaft 42 sprays into promotion blade 18 in non-turbine-type impeller 6 chamber and makes combined type acting rotor turns, high-temperature high-pressure fuel gas is enclosed in rotor cavity 43 by blade 18 and enters in chamber, whirlpool 9 with vane rotary drive turbine-type turbine 5 to rotate to cooled via return air road 21 during non-lower semi-circle air outlet 44, turbine-type impeller 6 chamber, high-temperature high-pressure fuel gas through guiding piece 54 lead after again dynamic impact problem turbine 59 make it rotate acting, waste gas after acting is discharged through main exhaust 20, combined type acting rotor is through acting rotor shaft 7, planetary gear set 10, rotor shaft 3 of calming the anger drives centrifugal compressor turbine 2 to rotate, power turbine 59 drives charging turbine 58 to rotate through supercharging rotor shaft 63, air enters in rotor of calming the anger through charging turbine 58 through suction port 8, guiding piece 54, the pressurized air with certain pressure is formed at air outlet 15 place after centrifugal compressor turbine 2 pressurizes, gas storage valve 34 cuts out caisson 35 and opens rotor air outlet 15 of calming the anger simultaneously, pressurized air enters through air outlet 15 in firing chamber rear chamber 26 and form inflammable mixture with high-temperature high-pressure fuel gas together burning expansion promotion combined type acting rotor and power turbine 59 rotation acting with the fuel mix of fuel injector 28 ejection from fumarole 27 Pen Ren firing chamber front chamber 25, acting rotor shaft 7 is through planetary gear set 10, basin tooth 61, cone tooth 62, power output shaft 60 output power.The secondary suction valve 41 on extra-air inlet 37 and the return-air valve 22 on return-air road 21 can also be closed, the bypass valve 13 opened on bypass air flue 12 closes the air throttle 14 on bypass air flue 12, open the outlet valve 46 on master air suction valve 40 and camshaft 42 on primary air inlet 36 and secondary air outlet flue 45, high-temperature high-pressure fuel gas is master air suction valve 40 on primary air inlet 36 all, camshaft 42 sprays into promotion blade 18 in non-turbine-type impeller 6 chamber and makes the acting of combined type acting rotor turns, waste gas after acting directly enters main exhaust 20 through secondary air outlet flue 45 and discharges, turbine-type turbine 5 rotates and makes to produce negative pressure in chamber, whirlpool 9, the bypass one-way valve 16 of air under the negative-pressure sucking in chamber, whirlpool 9 on bypass air flue 12 enters chamber, whirlpool through turbine-type turbine 5, guiding piece 54, the waste gas that power turbine 59 is discharged with secondary air outlet flue 45 from main exhaust 20 is discharged together.All right, close the secondary suction valve 41 on the master air suction valve 40 on primary air inlet 36 and the return-air valve 22 open auxiliary suction port 37 on return-air road 21, high-pressure gas all enters in chamber, whirlpool 9 through extra-air inlet 37 and drives turbine-type turbine 5, power turbine 59 rotates, and waste gas is discharged through main exhaust 20.All right, master air suction valve 40 on appropriate unlatching primary air inlet 36 and the secondary suction valve 41 on extra-air inlet 37, open the return-air valve 22 on return-air road 21, a part of high-pressure gas is allowed directly to enter chamber, whirlpool 9 through extra-air inlet 37, another part high-pressure gas enters in non-turbine-type impeller 6 chamber through primary air inlet 36 and promotes blade 18 and drive the combined type rotor that does work to rotate together, and the combustion gas cooled via return air road 21 after acting again enters chamber, whirlpool 9 and promotes turbine-type turbine 5 together with the high-pressure gas entering chamber, whirlpool 9 from extra-air inlet 37 and rotate acting.When the non-turbine-type impeller 6 that tongue piece 51 is housed works, the air inlet duct one-way valve 48 on air inlet duct 47 and the outgassing groove one-way valve 50 on outgassing groove 49 can also be opened, close the bypass valve 13 on chamber, whirlpool 9 bypass air flue 12 and air throttle 14, allow air under the pump of tongue piece 51 is inhaled through bypass one-way valve 16, air inlet duct 47 enters in rotor cavity 52, glide air in rotor cavity 52 through outgassing groove 49 under the compressing of tongue piece 51 at high-pressure gas when rotor cavity 52 goes to outgassing groove 49, outgassing groove one-way valve 50 enters in chamber, whirlpool 9, the Air flow combined type acting rotor making the temperature from air lower.All right, open the air throttle 14 on the air inlet duct one-way valve 48 on air inlet duct 47 and the outgassing groove one-way valve 50 on outgassing groove 49 and chamber, whirlpool 9 bypass air flue 12, close the bypass valve 13 on chamber, whirlpool 9 bypass air flue 12, allow from rotor air outlet 15 of calming the anger pressurized air tongue piece pump inhale under through bypass air flue 12, air inlet duct one-way valve 48, air inlet duct 47 enters in rotor cavity 52, when rotor cavity 52 goes to outgassing groove 49, tongue piece 51 glides rotor cavity 52 compressed air through outgassing groove 49 under the pressure effect of high-pressure gas, outgassing groove one-way valve 50 enters in chamber, whirlpool 9, the pressure-air cooling combined type acting rotor making the temperature from rotor of calming the anger relatively low.All right, open the bypass valve 13 on chamber, whirlpool 9 bypass air flue 12 and air throttle 14, allow part directly enter in chamber, whirlpool 9 from the pressurized air of 15 li, rotor air outlet of calming the anger and promote turbine-type page wheel 5 together with the mixed combustion of high-temperature high-pressure fuel gas and power turbine 59 rotates acting.Extra fuel sprays in bypass air flue 12 by the secondary fuel injector 28 ' can also opened on bypass air flue 12 follows the pressurized air mixing from 15 li, rotor air outlet of calming the anger to generate inflammable mixture to enter in chamber, whirlpool 9 to burn together with high-temperature high-pressure fuel gas and promote turbine-type turbine 5 and power turbine 59 rotates acting, secondary fuel injector 28 ' on open auxiliary suction port 37 extra fuel can also directly be sprayed into chamber, whirlpool 9 combustion through extra-air inlet 37, export more powerful power.When needs slow-speed of revolution low-power exports, in firing chamber rear chamber 26, telescopic pipe 32 extends and makes fuel injector 28 slide into front position forward in fumarole 27, make fumarole 27 aperture minimum, under identical working pressure, jet amount is minimum, fuel injector 28 sprays into minimum fuel, in firing chamber front chamber 25, gaseous-pressure is relatively low, close the secondary suction valve 41 on extra-air inlet 37 and the bypass valve 13 on chamber, whirlpool 9 bypass air flue 12, the relatively low pressure gas master air suction valve 40 on primary air inlet 36 of pressure enters in primary air inlet 36, rotating cam axle 42 turns suction port down makes pressure gas spray in non-turbine-type impeller 6 chamber with 90 degree of corner cuts, impacting blade 18 makes combined type rotate acting, combined type acting rotor rotates in the counterclockwise direction, high-pressure gas is enclosed in rotor cavity 43 to enter in chamber, whirlpool 9 with vane rotary to cooled via return air road, lower semi-circle air outlet 44 place, non-turbine-type impeller 6 chamber 21 by blade 18 and again drives turbine-type turbine 5 to rotate, power turbine 59 rotates, waste gas is discharged through main exhaust 20.When the high rotating speed low-power of needs exports, close secondary suction valve 41 on extra-air inlet 37 and the return-air valve 22 on return-air road 21 and the air throttle 14 on bypass air flue 12, outlet valve 46 on open auxiliary air outlet flue 45 and the bypass valve 13 on bypass air flue 12, telescopic pipe 32 retraction makes fuel injector 28 slide in fumarole 27 backward and strengthens fumarole 27 aperture in right amount, the pressurized gas sprayed in firing chamber front chamber 25 is increased, the appropriate increasing fuel straying quatity of fuel injector 28 simultaneously, the temperature of combustion gas in firing chamber front chamber 25, pressure raises simultaneously, rotating cam axle 42 strengthens suction port aperture in right amount, the high-pressure gas entered in non-turbine-type impeller 6 chamber increases, the thrust acted on blade 18 improves, combined type acting rotor speed improves, waste gas directly enters main exhaust 20 through secondary air outlet flue 45 and discharges, air is through bypass one-way valve 16, bypass air flue 12, bypass valve 13 enters behind chamber, whirlpool 9 again through turbine-type turbine 5, power turbine 59, second power turbine 59 ', 3rd power turbine 59 〞 enters main exhaust 20 and discharges.Also passable, close the secondary suction valve 41 on extra-air inlet 37 and the outlet valve 46 on secondary air outlet flue 45, open return-air valve 22 on return-air road 21 and the air throttle 14 on bypass air flue 12 and the bypass valve 13 on bypass air flue 12, allow telescopic pipe 32 bounce back and make fuel injector 28 fumarole 27 of the appropriate increasing of slip backward aperture in fumarole 27, the pressurized gas sprayed in firing chamber front chamber 25 is increased, the appropriate increasing fuel straying quatity of fuel injector 28 simultaneously, the temperature of combustion gas in firing chamber front chamber 25, pressure raises simultaneously, rotating cam axle 42 strengthens suction port aperture in right amount, the high-pressure gas entered in non-turbine-type impeller 6 chamber increases, the thrust acted on blade 18 improves, combined type acting rotor speed improves, in non-turbine-type impeller 6 chamber, the rear pressure gas of acting is through air outlet 44, return-air road 21 enters in chamber, whirlpool 9, the pressurized air of calming the anger in rotor air outlet 15 is through by-pass damper 14, bypass air flue 12, bypass valve 13 enters chamber, whirlpool 9 and promotes turbine-type turbine 5 together with chamber, whirlpool 9 internal pressure combustion gas, second turbine-type turbine 5 ', power turbine 59, second power turbine 59 ', 3rd power turbine 59 〞 rotates, the rear waste gas of acting enters main exhaust 20 and discharges.When the high-power output of the needs slow-speed of revolution, allow telescopic pipe 32 bounce back and make fuel injector 28 slip backward in fumarole 27 that fumarole 27 aperture is strengthened, the pressurized gas sprayed in firing chamber front chamber 25 increases, fuel injector 28 increasing fuel straying quatity simultaneously, the temperature of combustion gas in firing chamber front chamber 25, pressure significantly raises, the fuel that secondary suction valve 41 on appropriate open auxiliary suction port 37 and secondary fuel injector 28 ' allow partial high pressure combustion gas directly spray into secondary fuel injector 28 ' carries out mixing pre-burning and sprays into chamber, whirlpool 9 through extra-air inlet 37 and drive turbine-type turbine 5, second turbine-type turbine 5 ', power turbine 59, second power turbine 59 ', 3rd power turbine 59 〞 rotates, rotating cam axle 42 strengthens suction port aperture, the high-pressure gas entered in non-turbine-type impeller 6 chamber increases, the thrust acted on blade 18 improves, combined type acting rotor outputting torsion strengthens, waste gas is discharged through main exhaust 20.When the high-power output of the high rotating speed of needs, allow telescopic pipe 32 bounce back and make fuel injector 28 slip backward in fumarole 27 make fumarole 27 aperture maximum, the compression tolerance sprayed in firing chamber front chamber 25 is maximum, fuel injector 28 increasing fuel straying quatity simultaneously, the temperature of combustion gas in firing chamber front chamber 25, pressure significantly raises, outlet valve 46 on open auxiliary air outlet flue 45 and the bypass valve 13 in bypass air flue 12, secondary suction valve 41 standard-sized sheet on extra-air inlet 37 allows most of high-pressure gas directly enter chamber, whirlpool 9 through extra-air inlet 37, the fuel that secondary suction valve 41 on open auxiliary suction port 37 and secondary fuel injector 28 ' allow high-temperature high-pressure fuel gas directly spray into secondary fuel injector 28 ' carries out mixed combustion and sprays into chamber, whirlpool 9 through extra-air inlet 37, extra fuel sprays in bypass air flue 12 by the secondary fuel injector 28 ' opened on bypass air flue 12 follows the pressurized air mixing from 15 li, rotor air outlet of calming the anger to generate inflammable mixture to enter to burn together with high-temperature high-pressure fuel gas that the pre-mixing gas combustion that enters chamber, whirlpool 9 with extra-air inlet 37 in chamber, whirlpool 9 and return-air road 21 enter and promote turbine-type turbine 5, second turbine-type turbine 5 ', power turbine 59, second power turbine 59 ', 3rd power turbine 59 〞 rotates, waste gas after acting is discharged through main exhaust 20, combined type acting working rotor is at large torsion high-speed state, power output shaft 60 exports great power.

Fumarole 27 variable makes firing chamber rear chamber 26 under identical operating air pressure, spray into the controlled of compressed air stream quantitative change in firing chamber front chamber 25, the pressurized gas straying quatity sprayed in firing chamber front chamber 25 can be changed when without the need to changing pressure, also have, the variable combustion of the inflammable mixture/gas that makes of two items of fuel straying quatity and pressurized gas straying quatity is than more easy to control, under identical working pressure increasing output power namely improve in outputting torsion and the process of rotating speed can make the combustion/gas of inflammable mixture than relative remain in optimum value constant, this can only the internal-combustion engine of individual event change not accomplished, the ubiquitous phenomenon of internal-combustion engine that existing individual event changes is---emit a burst of dense smoke during acceleration, have plenty of by reducing acceleration to improve this defect, also have, when the timing of fumarole 27 size one, under identical working pressure, jet amount is certain, under identical working pressure, its power range is just limited at maximum combustion/gas of inflammable mixture than following between minimum combustion/gas ratio, two items of fuel straying quatity and pressurized gas straying quatity are variable power stage scope is become wider, also have, in work when load increases, its rotating speed reduces, amount of consumed gas reduces, in firing chamber front chamber 25, gaseous-pressure rising makes piston 23 slide toward rear chamber 26, reduce fumarole 27 aperture, reduce pressurized gas straying quatity, combustion/gas the ratio of inflammable mixture is improve under equal fuel straying quatity, the simultaneous temperature and the pressure that export gas quantity minimizing in firing chamber front chamber 25 raise, the active force acted on blade 18 raises, combined type acting rotor speed raises, amount of consumed gas raises, in firing chamber front chamber 25, gaseous-pressure declines, piston 23 slides toward front chamber 25 under the pressure of spring 30 and pressurized gas, fumarole 27 aperture increases, pressurized gas straying quatity increases, combustion/gas the ratio of inflammable mixture is reduced under equal fuel straying quatity, in firing chamber front chamber 25, while temperature and pressure reduction, combustion gas output quantity increases, make it have very high adaptive ability, telescopic pipe 32 makes fuel obtain good preheating in the process by telescopic pipe 32 in firing chamber rear chamber 26, also have, can spring 30 be promoted by piston position controller 31 or pull the position of spring 30 pairs of pistons 23 to adjust, as: when use hydrogen, liquid gas, rock gas, during the gaseous fuels such as coal gas, due to the diffusivity of gaseous fuel, flammability is all relatively high, spring 30 can be promoted with piston position controller 31 and piston 23 is pushed into forward position relatively before examination, firing chamber front chamber 25 front end, make the capacity relative of firing chamber front chamber 25 less, make piston 23 the shortest to the distance of combined type acting rotor main suction port 36 and extra-air inlet 37, when use gasoline, light kerosene, during the volatile liquid fuel such as alcohol, due to the diffusivity of this class A fuel A, flammability is high, spring 30 can be pulled piston 23 to be adjusted back to relative middle section position before and after in firing chamber between chamber with piston position controller 31, extend the distance that piston 23 arrives combined type acting rotor main suction port 36 and extra-air inlet 37, when use kerosene, during the not volatile heavy class A fuel A such as diesel oil, spring 30 can be pulled piston 23 to be adjusted back in firing chamber in rear chamber 26 position more rearward with piston position controller 31, make length in firing chamber front chamber 25 relatively long, extend fuel from injection, be mixed into the distance of burning, relatively extend fuel to do time in advance with compressed-air actuated, also have, pressurized air in firing chamber rear chamber 26 is when fumarole 27 sprays into firing chamber front chamber 25, spray in the shape of a spiral in firing chamber front chamber 25 by several angle under the guide functions of pressurized air guiding piece 29 in fumarole 27 and form eddy current, extend fuel relatively further from injection, be mixed into the distance of burning, extend fuel relatively further and improve mixture homogeneity the diffusion time in pressurized gas, make fuel combustion more abundant, it is wider that firing chamber variable adjustable controlled makes fuel Applicable scope become, utilize and rearmountedly can the turbine flow of independence and freedom running drive charging turbine can farthest allow the transformation of energy in combustion gas become useful work, make waste gas flow velocity and temperature after acting all very low, improve efficiency, the optional machine that makes of multiple-working mode is at height, steadily reliable in low-speed running, make power stage scope wider, gas storage valve 34 and caisson 35 make startup simpler and easy and can store up in work calm the anger rotor produce excessive condensation gas can discharge booster engine work more when needed, play energy-conservation object.

By finding out describing of above five specific embodiments, the application can have many changes to be not limited only to above five specific embodiments, can exchange between above five specific embodiments with or without, mutual exchange, also have described combined type acting rotor can be one, two, or two or more multiple combined type acting rotor, also have, it also can be that the private firing chamber of each acting rotor can also divide into groups to use firing chamber that described multiple combined type acting rotor can share a firing chamber, described rotor of calming the anger can be by centrifugal turbocompressor, blade pump type gas compressor, turbine-type hinge gas compressor combines, also can be that other form being applicable to this programme is calmed the anger rotor, described rotor of calming the anger can also be one-level, two-stage or the above multistage compressor structure of two-stage, as multistage turbine gas compressor, multistage blade gas compressor etc., described rotor of calming the anger can also be the combined multi-stage gas pressure mechanism that the gas compressor of various ways is formed, be final stage as made primary centrifugal turbocompressor with turbine hinge formula gas compressor, centrifugal turbocompressor is primary blades pump type gas compressor is the mixed construction such as middle final stage, described multistage compressor structure or hybrid multi-stage gas pressure mechanism at different levels between can be can also be that selectively to use planetary gear set to carry out connection coaxial by the split axle pattern that planetary gear set connects, split axle mixed mode, described planetary gear set can be single planetary gear set structure also can be many planetary structures that two or more multiple planetary gear set are formed, can be electronic by routine of the prior art--mechanically activated, above all changes are all within the application's protection domain.

Claims

1. an internal-combustion engine, by body, to calm the anger rotor, acting rotor, firing chamber and fuel supplying device, ignition mechanism is formed, rotor of calming the anger is arranged in body respectively with acting rotor calms the anger in rotor chamber and acting rotor chamber, body there is interval body wall, guiding piece, hollow spacer dish and spring bearing, it is characterized in that: described in calm the anger rotor and acting rotor in body on same axis, described rotor of calming the anger is made up of centrifugal compressor turbine and charging turbine, described centrifugal compressor turbine is arranged on rotor shaft front end of calming the anger, described acting rotor is made up of combined type acting rotor and power turbine, described combined type acting rotor is by conical wheel body, turbine-type turbine and non-turbine-type impeller are formed, the conical wheel body of described combined type acting rotor is arranged on acting rotor shaft rear end, described conical wheel body excircle is turbine-type turbine, described turbine-type turbine excircle is non-turbine-type blade wheel structure, the chamber, bowl-type whirlpool matched with turbine-type turbine diameter is had before the turbine-type turbine of described combined type acting rotor, described acting rotor shaft front end is passed Wo Qiang bottom centre and is connected with rotor shaft rear end of calming the anger and connect with power output shaft through gearing, described acting rotor shaft is with calming the anger rotor shaft on same center line, described centrifugal compressor turbine is arranged on rotor shaft front end of calming the anger, described charging turbine is arranged on supercharging rotor shaft front end, described supercharging rotor shaft rear end to be contained in rotor beam barrel of calming the anger through centrifugal compressor turbine central sleeve and to pass acting rotor shaft rear end, described power turbine is arranged on calm the anger rotor shaft and the supercharging rotor shaft rear end that passes, acting rotor shaft center, centrifugal compressor turbine with between charging turbine and the turbine-type turbine of combined type acting rotor have guiding piece and hollow spacer dish with between power turbine, described guiding piece outer end is fixed on body, the main exhaust matched with power turbine diameter is had after power turbine, combuster on combined type acting rotor, described firing chamber there are fuel supplying device and ignition mechanism, rear end, described firing chamber communicates with rotor air outlet of calming the anger, described chamber front end has combined type acting rotor main suction port and extra-air inlet, described primary air inlet communicates with non-turbine-type impeller cavity on the non-turbine-type impeller cavity upper semi-circle of combined type acting rotor, described extra-air inlet is communicated with the chamber, whirlpool before the turbine-type turbine of combined type acting rotor, the lower semi-circle that described combined type acting rotor non-turbine-type impeller cavity suction port is relative there is acting rotor air outlet, described acting rotor air outlet there is return-air road and communicate with return-air road, described return-air road is communicated with the chamber, whirlpool before combined type acting rotor turbine-type turbine, chamber, whirlpool before described combined type acting rotor turbine-type turbine also communicates with the main exhaust after power turbine through turbine-type turbine and power turbine.

2. a kind of internal-combustion engine according to claim 1, it is characterized in that: described charging turbine is the multi-stage booster turbine be made up of multiple charging turbine, described power turbine is the turbine flow be made up of multiple power turbine, the first charging turbine in described multi-stage booster turbine is arranged on the first supercharging rotor shaft front end, described first supercharging rotor shaft rear end through centrifugal compressor turbine center and to be sleeved in the beam barrel of rotor shaft of calming the anger and to pass the rear end of acting rotor shaft and the first power turbine is installed, second charging turbine is arranged on the second supercharging rotor shaft front end, described second supercharging rotor shaft rear end through the first charging turbine center and to be sleeved in the beam barrel of the first supercharging rotor shaft and after passing the first supercharging rotor shaft, the second power turbine to be installed, 3rd charging turbine is arranged on the 3rd supercharging rotor shaft front end, the rear end of described 3rd supercharging rotor shaft to be contained in the beam barrel of the second supercharging rotor shaft through the second charging turbine central sleeve and to be provided with the 3rd power turbine after passing the second supercharging rotor beam barrel, charging turbines at different levels in described multi-stage booster turbine are arranged on the front end of supercharging rotor shaft at different levels successively, the rear end of described supercharging rotor shaft at different levels to be contained in the beam barrel of prime supercharging rotor shaft through prime charging turbine central sleeve and to be provided with corresponding power turbine at the corresponding levels after passing prime supercharging rotor beam barrel, centrifugal compressor turbine with between the first charging turbine and between the adjacent two-stage in multi-stage booster turbine and the turbine-type turbine of combined type acting rotor with between the first power turbine and have corresponding guiding piece and hollow spacer dish between the adjacent two-stage in turbine flow, described guiding piece outer end is fixed on body, the inner is fixed on hollow spacer dish excircle, described guiding piece angle of yaw is with centrifugal compressor turbine, charging turbine at different levels, the angle of yaw of the acting turbine-type turbine of rotor and power turbine at different levels is contrary, the main exhaust having diameter to follow final stage power turbine diameter after the final stage power turbine of described turbine flow to match, described acting rotor air outlet in combined type acting rotor non-turbine-type impeller cavity lower semi-circle circumferentially, described acting rotor air outlet there are return-air road and secondary air outlet flue, described return-air road there is return-air valve, described combined type acting rotor air outlet, outside return-air road, secondary air outlet flue there is outlet valve, described secondary air outlet flue is communicated with main exhaust through outlet valve, chamber, whirlpool before described combined type acting rotor turbine-type turbine communicates with the main exhaust after the final stage power turbine of turbine flow through turbine-type turbine and turbine flow.

3. a kind of internal-combustion engine according to claim 1, it is characterized in that: described combined type acting rotor non-turbine-type impeller has with blade with wide tongue piece between adjacent two blades, a limit of described tongue piece with a blade top margin in adjacent two blades through the Viability connection of movable axis, described tongue piece is that the blade face of its another edge another blade adjacent of axle center slides up and down in scope between zero to nine ten degree with movable axis, its top dead center is no more than the corresponding blade top margin slided, its radian of blade face camber corresponding to described tongue piece sliding edge and the slip radian of tongue piece sliding edge match, described tongue piece active edges is adjacent two blades when top dead center, chamber wall, the rotor cavity forming an opposing seal between week is taken turns in tongue piece and blade place.

4. a kind of internal-combustion engine according to claim 1, it is characterized in that: described firing chamber has the cylindrical piston matched with circular diameter in firing chamber in cylindrical shape, described cylindrical piston periphery there is seal ring, described cylindrical piston is divided into firing chamber front chamber and firing chamber rear chamber firing chamber, described cylindrical piston slides in the front and back chamber of firing chamber, there is fumarole at described cylindrical piston center, described fumarole center is built with fuel injector, described fuel injector slides axially in fumarole, piston position controller is had in described cylindrical piston rear end firing chamber rear chamber, telescopic pipe is had in described firing chamber rear chamber, described telescopic pipe front end communicates with fuel injector, rear end communicates through piston position controller and body heel fuel supplying device, described firing chamber rear chamber rear end is communicated with rotor air outlet of calming the anger, described firing chamber front chamber front end communicates with combined type acting rotor main suction port and extra-air inlet.

5. a kind of internal-combustion engine according to claim 1, is characterized in that: there are gas-separating valve in described combined type acting rotor main suction port and extra-air inlet intersection.

6. a kind of internal-combustion engine according to claim 1, is characterized in that: described combined type acting rotor main suction port and extra-air inlet are equipped with master air suction valve and secondary suction valve respectively.

7. a kind of internal-combustion engine according to claim 1, it is characterized in that: described acting rotor shaft front end connects through planetary gear set with rotor shaft rear end of calming the anger through Wo Qiang bottom centre, described planetary gear set connects with power output shaft through gearing, described planetary gear set has planetary gear set control gear.

8. a kind of internal-combustion engine according to any one of claim 1 to 7, it is characterized in that: described gearing is the gear train be made up of basin heel cone tooth, described rotor air outlet of calming the anger there is gas storage valve, described gas storage valve is communicated with the outer caisson of body, described combined type acting rotor non-turbo wheel chamber there is rotating camshaft in primary air inlet, in described firing chamber front chamber front end, there is flameholder in combined type acting rotor main suction port and extra-air inlet front, spring is had between cylindrical piston rear end and piston position controller in described firing chamber, described acting rotor shaft is followed between supercharging rotor shaft and is had spring bearing between supercharging rotor shaft at different levels.

9. a kind of internal-combustion engine according to claim 3, it is characterized in that: below described combined type acting rotor non-turbine-type impeller cavity suction port, sidewall has with circular arc air inlet duct corresponding to chamber, bowl-type whirlpool circular arc degree, lower semi-circle sidewall has corresponding circular arc outgassing groove, chamber, whirlpool before described combined type acting rotor turbine-type turbine has bypass air flue to communicate with calm the anger rotor air outlet and air, described bypass air flue communicates with rotor air outlet of calming the anger through bypass valve, described bypass air flue there is one-way valve with the air place of communicating, pore is had to follow the circular arc outgassing groove on combined type acting rotor non-turbine-type impeller cavity sidewall and circular arc air inlet duct to communicate bottom described rotor cavity, described outgassing groove communicates with chamber, bowl-type whirlpool, described air inlet duct is communicated with between one-way valve and bypass valve with the bypass air flue in chamber, bowl-type whirlpool, secondary fuel injector is had on described bypass valve internal bypass air flue He on secondary intake duct, described secondary fuel injector is communicated with fuel supplying device.

10. a kind of internal-combustion engine according to claim 9, is characterized in that: the air flue that described air inlet duct communicates with bypass air flue has one-way valve, and the air flue that described outgassing groove communicates with chamber, whirlpool has one-way valve.